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CConfig Class Reference

Main class for defining the problem; basically this class reads the configuration file, and stores all the information. More...

#include <config_structure.hpp>

Public Member Functions

 CConfig (char case_filename[MAX_STRING_SIZE], unsigned short val_software, unsigned short val_iZone, unsigned short val_nZone, unsigned short val_nDim, unsigned short verb_level)
 Constructor of the class which reads the input file. More...
 
 CConfig (char case_filename[MAX_STRING_SIZE], unsigned short val_software)
 Constructor of the class which reads the input file. More...
 
 CConfig (char case_filename[MAX_STRING_SIZE], CConfig *config)
 Constructor of the class which reads the input file. More...
 
 ~CConfig (void)
 Destructor of the class. More...
 
SU2_MPI::Comm GetMPICommunicator ()
 Get the MPI communicator of SU2. More...
 
void SetMPICommunicator (SU2_MPI::Comm Communicator)
 Set the MPI communicator for SU2. More...
 
void SetPointersNull (void)
 Initializes pointers to null. More...
 
bool TokenizeString (string &str, string &option_name, vector< string > &option_value)
 breaks an input line from the config file into a set of tokens More...
 
su2doubleGetRefOriginMoment (unsigned short val_marker)
 Get reference origin for moment computation. More...
 
su2double GetRefOriginMoment_X (unsigned short val_marker)
 Get reference origin x-coordinate for moment computation. More...
 
su2double GetRefOriginMoment_Y (unsigned short val_marker)
 Get reference origin y-coordinate for moment computation. More...
 
su2double GetRefOriginMoment_Z (unsigned short val_marker)
 Get reference origin z-coordinate for moment computation. More...
 
void SetRefOriginMoment_X (unsigned short val_marker, su2double val_origin)
 Set reference origin x-coordinate for moment computation. More...
 
void SetRefOriginMoment_Y (unsigned short val_marker, su2double val_origin)
 Set reference origin y-coordinate for moment computation. More...
 
void SetRefOriginMoment_Z (unsigned short val_marker, su2double val_origin)
 Set reference origin z-coordinate for moment computation. More...
 
string GetPlaneTag (unsigned short index)
 Get index of the upper and lower horizontal plane. More...
 
su2double GetEA_IntLimit (unsigned short index)
 Get the integration limits for the equivalent area computation. More...
 
su2double GetEA_ScaleFactor (void)
 Get the integration limits for the equivalent area computation. More...
 
su2double GetAdjointLimit (void)
 Get the limit value for the adjoint variables. More...
 
su2doubleGetHold_GridFixed_Coord (void)
 Get the the coordinates where of the box where the grid is going to be deformed. More...
 
su2doubleGetSubsonicEngine_Values (void)
 Get the the coordinates where of the box where a subsonic region is imposed. More...
 
su2doubleGetSubsonicEngine_Cyl (void)
 Get the the coordinates where of the box where a subsonic region is imposed. More...
 
su2doubleGetDistortionRack (void)
 Get the the coordinates where of the box where a subsonic region is imposed. More...
 
su2double GetDualVol_Power (void)
 Get the power of the dual volume in the grid adaptation sensor. More...
 
unsigned short GetAnalytical_Surface (void)
 Get Information about if there is an analytical definition of the surface for doing the grid adaptation. More...
 
unsigned short GetGeo_Description (void)
 Get Description of the geometry to be analyzed. More...
 
bool GetExtraOutput (void)
 Creates a tecplot file to visualize the partition made by the DDC software. More...
 
long GetExtraHeatOutputZone (void)
 Heat solver zone with extra screen output. More...
 
su2double GetMach (void)
 Get the value of the Mach number (velocity divided by speed of sound). More...
 
su2double GetGamma (void)
 Get the value of the Gamma of fluid (ratio of specific heats). More...
 
su2double GetCFL_AdaptParam (unsigned short val_index)
 Get the values of the CFL adapation. More...
 
bool GetCFL_Adapt (void)
 Get the values of the CFL adapation. More...
 
su2double GetHTP_Axis (unsigned short val_index)
 Get the values of the CFL adapation. More...
 
su2double GetStations_Bounds (unsigned short val_var)
 Get the value of the limits for the sections. More...
 
su2double GetFFD_Axis (unsigned short val_var)
 Get the value of the vector that connects the cartesian axis with a sherical or cylindrical one. More...
 
su2double GetBulk_Modulus (void)
 Get the value of the bulk modulus. More...
 
su2double GetBeta_Factor (void)
 Get the epsilon^2 multiplier for Beta in the incompressible preconditioner. More...
 
su2double GetGas_Constant (void)
 Get the value of specific gas constant. More...
 
su2double GetGas_ConstantND (void)
 Get the value of specific gas constant. More...
 
su2double GetMolecular_Weight (void)
 Get the value of the molecular weight for an incompressible ideal gas (g/mol). More...
 
su2double GetSpecific_Heat_Cp (void)
 Get the value of specific heat at constant pressure. More...
 
su2double GetSpecific_Heat_Cp_Solid (void)
 Get the value of the specific heat for solids. More...
 
su2double GetSpecific_Heat_CpND (void)
 Get the non-dimensional value of specific heat at constant pressure. More...
 
su2double GetSpecific_Heat_Cv (void)
 Get the value of specific heat at constant volume. More...
 
su2double GetSpecific_Heat_CvND (void)
 Get the non-dimensional value of specific heat at constant volume. More...
 
su2double GetBlottnerCoeff (unsigned short val_Species, unsigned short val_Coeff)
 Get the coefficients of the Blottner viscosity model. More...
 
su2double GetPnormHeat (void)
 Get the p-norm for heat-flux objective functions (adjoint problem). More...
 
su2double GetWallTemperature (void)
 Get the value of wall temperature. More...
 
su2double GetGas_Constant_Ref (void)
 Get the reference value for the specific gas constant. More...
 
su2double GetHeat_Flux_Ref (void)
 Get the reference value for the heat flux. More...
 
su2double GetTemperature_FreeStream (void)
 Get the value of the frestream temperature. More...
 
su2double GetEnergy_FreeStream (void)
 Get the value of the frestream temperature. More...
 
su2double GetViscosity_FreeStream (void)
 Get the value of the frestream temperature. More...
 
su2double GetDensity_FreeStream (void)
 Get the value of the frestream temperature. More...
 
su2double GetDensity_Solid (void)
 Get the value of the solid density. More...
 
su2double GetModVel_FreeStream (void)
 Get the value of the frestream temperature. More...
 
su2double GetModVel_FreeStreamND (void)
 Get the value of the frestream temperature. More...
 
su2double GetTemperature_ve_FreeStream (void)
 Get the value of the frestream vibrational-electronic temperature. More...
 
su2double GetPrandtl_Lam (void)
 Get the value of the laminar Prandtl number. More...
 
su2double GetPrandtl_Turb (void)
 Get the value of the turbulent Prandtl number. More...
 
su2double GetThermalConductivity_Solid (void)
 Get the value of the thermal conductivity for solids. More...
 
su2double GetThermalDiffusivity_Solid (void)
 Get the value of the thermal diffusivity for solids. More...
 
su2double GetTemperature_Freestream_Solid (void)
 Get the temperature in solids at freestream conditions. More...
 
su2double GetLength_Ref (void)
 Get the value of the reference length for non-dimensionalization. This value should always be 1 internally, and is not user-specified. More...
 
su2double GetPressure_Ref (void)
 Get the value of the reference pressure for non-dimensionalization. More...
 
su2double GetEnergy_Ref (void)
 Get the value of the reference pressure for non-dimensionalization. More...
 
su2double GetTemperature_Ref (void)
 Get the value of the reference temperature for non-dimensionalization. More...
 
su2double GetDensity_Ref (void)
 Get the value of the reference density for non-dimensionalization. More...
 
su2double GetVelocity_Ref (void)
 Get the value of the reference velocity for non-dimensionalization. More...
 
su2double GetTime_Ref (void)
 Get the value of the reference time for non-dimensionalization. More...
 
su2double GetViscosity_Ref (void)
 Get the value of the reference viscosity for non-dimensionalization. More...
 
su2double GetHighlite_Area (void)
 Get the value of the reference viscosity for non-dimensionalization. More...
 
su2double GetFan_Poly_Eff (void)
 Get the value of the reference viscosity for non-dimensionalization. More...
 
su2double GetConductivity_Ref (void)
 Get the value of the reference conductivity for non-dimensionalization. More...
 
su2double GetOmega_Ref (void)
 Get the value of the reference angular velocity for non-dimensionalization. More...
 
su2double GetForce_Ref (void)
 Get the value of the reference force for non-dimensionalization. More...
 
su2double GetPressure_FreeStream (void)
 Get the value of the non-dimensionalized freestream pressure. More...
 
su2double GetPressure_FreeStreamND (void)
 Get the value of the non-dimensionalized freestream pressure. More...
 
su2double GetPressure_Thermodynamic (void)
 Get the value of the thermodynamic pressure. More...
 
su2double GetPressure_ThermodynamicND (void)
 Get the value of the non-dimensionalized thermodynamic pressure. More...
 
su2doubleGetVelocity_FreeStream (void)
 Get the vector of the dimensionalized freestream velocity. More...
 
su2double GetTemperature_FreeStreamND (void)
 Get the value of the non-dimensionalized freestream temperature. More...
 
su2double GetDensity_FreeStreamND (void)
 Get the value of the non-dimensionalized freestream density. More...
 
su2doubleGetVelocity_FreeStreamND (void)
 Get the vector of the non-dimensionalized freestream velocity. More...
 
su2double GetEnergy_FreeStreamND (void)
 Get the value of the non-dimensionalized freestream energy. More...
 
su2double GetViscosity_FreeStreamND (void)
 Get the value of the non-dimensionalized freestream viscosity. More...
 
su2double GetTke_FreeStreamND (void)
 Get the value of the non-dimensionalized freestream viscosity. More...
 
su2double GetOmega_FreeStreamND (void)
 Get the value of the non-dimensionalized freestream viscosity. More...
 
su2double GetTke_FreeStream (void)
 Get the value of the non-dimensionalized freestream viscosity. More...
 
su2double GetOmega_FreeStream (void)
 Get the value of the non-dimensionalized freestream viscosity. More...
 
su2double GetIntermittency_FreeStream (void)
 Get the value of the non-dimensionalized freestream intermittency. More...
 
su2double GetTurbulenceIntensity_FreeStream (void)
 Get the value of the non-dimensionalized freestream turbulence intensity. More...
 
su2double GetNuFactor_FreeStream (void)
 Get the value of the non-dimensionalized freestream turbulence intensity. More...
 
su2double GetNuFactor_Engine (void)
 Get the value of the non-dimensionalized engine turbulence intensity. More...
 
su2double GetSecondaryFlow_ActDisk (void)
 Get the value of the non-dimensionalized actuator disk turbulence intensity. More...
 
su2double GetInitial_BCThrust (void)
 Get the value of the non-dimensionalized actuator disk turbulence intensity. More...
 
void SetInitial_BCThrust (su2double val_bcthrust)
 Get the value of the non-dimensionalized actuator disk turbulence intensity. More...
 
su2double GetTurb2LamViscRatio_FreeStream (void)
 Get the value of the turbulent to laminar viscosity ratio. More...
 
su2doubleGetMassFrac_FreeStream (void)
 Get the vector of free stream mass fraction values. More...
 
su2double GetLength_Reynolds (void)
 Get the value of the Reynolds length. More...
 
unsigned short GetnStartUpIter (void)
 Get the start up iterations using the fine grid, this works only for multigrid problems. More...
 
su2double GetRefArea (void)
 Get the reference area for non dimensional coefficient computation. If the value from the is 0 then, the code will compute the reference area using the projection of the shape into the z plane (3D) or the x plane (2D). More...
 
su2double GetThermalDiffusivity (void)
 Get the wave speed. More...
 
su2double GetThermal_Expansion_Coeff (void)
 Get the thermal expansion coefficient. More...
 
su2double GetThermal_Expansion_CoeffND (void)
 Get the non-dim. thermal expansion coefficient. More...
 
void SetThermal_Expansion_Coeff (su2double val_thermal_expansion)
 Set the thermal expansion coefficient. More...
 
void SetThermal_Expansion_CoeffND (su2double val_thermal_expansionnd)
 Set the non-dim. thermal expansion coefficient. More...
 
su2double GetInc_Density_Ref (void)
 Get the value of the reference density for custom incompressible non-dimensionalization. More...
 
su2double GetInc_Velocity_Ref (void)
 Get the value of the reference velocity for custom incompressible non-dimensionalization. More...
 
su2double GetInc_Temperature_Ref (void)
 Get the value of the reference temperature for custom incompressible non-dimensionalization. More...
 
su2double GetInc_Density_Init (void)
 Get the value of the initial density for incompressible flows. More...
 
su2doubleGetInc_Velocity_Init (void)
 Get the value of the initial velocity for incompressible flows. More...
 
su2double GetInc_Temperature_Init (void)
 Get the value of the initial temperature for incompressible flows. More...
 
su2double GetElasticyMod (unsigned short id_val)
 Get the Young's modulus of elasticity. More...
 
bool GetDE_Effects (void)
 Decide whether to apply DE effects to the model. More...
 
bool GetDE_Predicted (void)
 Decide whether to predict the DE effects for the next time step. More...
 
unsigned short GetnElectric_Constant (void)
 Get the number of different electric constants. More...
 
su2double GetElectric_Constant (unsigned short iVar)
 Get the value of the DE modulus. More...
 
su2double GetKnowles_B (void)
 Get the value of the B constant in the Knowles material model. More...
 
su2double GetKnowles_N (void)
 Get the value of the N constant in the Knowles material model. More...
 
unsigned short GetDV_FEA (void)
 Get the kind of design variable for FEA. More...
 
unsigned long GetRefNode_ID (void)
 Get the ID of the reference node. More...
 
su2double GetRefNode_Displacement (unsigned short val_coeff)
 Get the values for the reference node displacement. More...
 
su2double GetRefNode_Penalty (void)
 Get the penalty weight value for the objective function. More...
 
bool GetRefGeom (void)
 Decide whether it's necessary to read a reference geometry. More...
 
string GetRefGeom_FEMFileName (void)
 Get the name of the file with the reference geometry of the structural problem. More...
 
unsigned short GetRefGeom_FileFormat (void)
 Get the format of the reference geometry file. More...
 
unsigned short GetElas2D_Formulation (void)
 Formulation for 2D elasticity (plane stress - strain) More...
 
bool GetPrestretch (void)
 Decide whether it's necessary to read a reference geometry. More...
 
bool Add_CrossTerm (void)
 Decide whether it's necessary to add the cross term for adjoint FSI. More...
 
void Set_CrossTerm (bool needCrossTerm)
 Set the boolean addCrossTerm to true or false. More...
 
string GetFEA_FileName (void)
 Get the name of the file with the element properties for structural problems. More...
 
string GetPrestretch_FEMFileName (void)
 Get the name of the file with the reference geometry of the structural problem. More...
 
su2double GetPoissonRatio (unsigned short id_val)
 Get the Poisson's ratio. More...
 
su2double GetMaterialDensity (unsigned short id_val)
 Get the Material Density. More...
 
unsigned short GetMaterialCompressibility (void)
 Compressibility/incompressibility of the solids analysed using the structural solver. More...
 
unsigned short GetMaterialModel (void)
 Compressibility/incompressibility of the solids analysed using the structural solver. More...
 
unsigned short GetGeometricConditions (void)
 Geometric conditions for the structural solver. More...
 
su2double GetRefLength (void)
 Get the reference length for computing moment (the default value is 1). More...
 
su2double GetRefElemLength (void)
 Get the reference element length for computing the slope limiting epsilon. More...
 
su2double GetRefSharpEdges (void)
 Get the reference coefficient for detecting sharp edges. More...
 
su2double GetDomainVolume (void)
 Get the volume of the whole domain using the fine grid, this value is common for all the grids in the multigrid method. More...
 
void SetRefArea (su2double val_area)
 In case the RefArea is equal to 0 then, it is necessary to compute a reference area, with this function we set the value of the reference area. More...
 
void SetSemiSpan (su2double val_semispan)
 In case the SemiSpan is equal to 0 then, it is necessary to compute the max y distance, with this function we set the value of the semi span. More...
 
void SetDomainVolume (su2double val_volume)
 Set the value of the domain volume computed on the finest grid. More...
 
void SetFinestMesh (unsigned short val_finestmesh)
 Set the finest mesh in a multigrid strategy. More...
 
void SetKind_TimeIntScheme (unsigned short val_kind_timeintscheme)
 Set the kind of time integration scheme. More...
 
void SetKind_ConvNumScheme (unsigned short val_kind_convnumscheme, unsigned short val_kind_centered, unsigned short val_kind_upwind, unsigned short val_kind_slopelimit, bool val_muscl, unsigned short val_kind_fem)
 Set the parameters of the convective numerical scheme. More...
 
su2double GetVenkat_LimiterCoeff (void)
 Get the value of limiter coefficient. More...
 
unsigned long GetLimiterIter (void)
 Freeze the value of the limiter after a number of iterations. More...
 
su2double GetAdjSharp_LimiterCoeff (void)
 Get the value of sharp edge limiter. More...
 
su2double GetReynolds (void)
 Get the Reynolds number. Dimensionless number that gives a measure of the ratio of inertial forces to viscous forces and consequently quantifies the relative importance of these two types of forces for given flow condition. More...
 
su2double GetFroude (void)
 Get the Froude number for free surface problems. More...
 
void SetFroude (su2double val_froude)
 Set the Froude number for free surface problems. More...
 
void SetMach (su2double val_mach)
 Set the Froude number for free surface problems. More...
 
void SetReynolds (su2double val_reynolds)
 Set the Froude number for free surface problems. More...
 
void SetLength_Ref (su2double val_length_ref)
 Set the Froude number for free surface problems. More...
 
void SetVelocity_Ref (su2double val_velocity_ref)
 Set the Froude number for free surface problems. More...
 
void SetPressure_Ref (su2double val_pressure_ref)
 Set the Froude number for free surface problems. More...
 
void SetDensity_Ref (su2double val_density_ref)
 Set the Froude number for free surface problems. More...
 
void SetTemperature_Ref (su2double val_temperature_ref)
 Set the reference temperature. More...
 
void SetTime_Ref (su2double val_time_ref)
 Set the Froude number for free surface problems. More...
 
void SetEnergy_Ref (su2double val_energy_ref)
 Set the Froude number for free surface problems. More...
 
void SetOmega_Ref (su2double val_omega_ref)
 Set the Froude number for free surface problems. More...
 
void SetForce_Ref (su2double val_force_ref)
 Set the Froude number for free surface problems. More...
 
void SetGas_Constant_Ref (su2double val_gas_constant_ref)
 Set the Froude number for free surface problems. More...
 
void SetGas_Constant (su2double val_gas_constant)
 Set the Froude number for free surface problems. More...
 
void SetSpecific_Heat_Cp (su2double val_specific_heat_cp)
 Set the value of the specific heat at constant pressure (incompressible fluids with energy equation). More...
 
void SetSpecific_Heat_CpND (su2double val_specific_heat_cpnd)
 Set the non-dimensional value of the specific heat at constant pressure (incompressible fluids with energy equation). More...
 
void SetSpecific_Heat_Cv (su2double val_specific_heat_cv)
 Set the value of the specific heat at constant volume (incompressible fluids with energy equation). More...
 
void SetSpecific_Heat_CvND (su2double val_specific_heat_cvnd)
 Set the non-dimensional value of the specific heat at constant volume (incompressible fluids with energy equation). More...
 
void SetHeat_Flux_Ref (su2double val_heat_flux_ref)
 Set the heat flux reference value. More...
 
void SetViscosity_Ref (su2double val_viscosity_ref)
 Set the Froude number for free surface problems. More...
 
void SetConductivity_Ref (su2double val_conductivity_ref)
 Set the Froude number for free surface problems. More...
 
void SetPressure_FreeStreamND (su2double val_pressure_freestreamnd)
 Set the Froude number for free surface problems. More...
 
void SetPressure_FreeStream (su2double val_pressure_freestream)
 Set the Froude number for free surface problems. More...
 
void SetPressure_ThermodynamicND (su2double val_pressure_thermodynamicnd)
 Set the non-dimensionalized thermodynamic pressure for low Mach problems. More...
 
void SetPressure_Thermodynamic (su2double val_pressure_thermodynamic)
 Set the thermodynamic pressure for low Mach problems. More...
 
void SetDensity_FreeStreamND (su2double val_density_freestreamnd)
 Set the Froude number for free surface problems. More...
 
void SetDensity_FreeStream (su2double val_density_freestream)
 Set the Froude number for free surface problems. More...
 
void SetViscosity_FreeStream (su2double val_viscosity_freestream)
 Set the Froude number for free surface problems. More...
 
void SetModVel_FreeStream (su2double val_modvel_freestream)
 Set the Froude number for free surface problems. More...
 
void SetModVel_FreeStreamND (su2double val_modvel_freestreamnd)
 Set the Froude number for free surface problems. More...
 
void SetTemperature_FreeStream (su2double val_temperature_freestream)
 Set the Froude number for free surface problems. More...
 
void SetTemperature_FreeStreamND (su2double val_temperature_freestreamnd)
 Set the Froude number for free surface problems. More...
 
void SetGas_ConstantND (su2double val_gas_constantnd)
 Set the Froude number for free surface problems. More...
 
void SetVelocity_FreeStream (su2double val_velocity_freestream, unsigned short val_dim)
 Set the free-stream velocity. More...
 
void SetVelocity_FreeStreamND (su2double val_velocity_freestreamnd, unsigned short val_dim)
 Set the Froude number for free surface problems. More...
 
void SetViscosity_FreeStreamND (su2double val_viscosity_freestreamnd)
 Set the Froude number for free surface problems. More...
 
void SetTke_FreeStreamND (su2double val_tke_freestreamnd)
 Set the Froude number for free surface problems. More...
 
void SetOmega_FreeStreamND (su2double val_omega_freestreamnd)
 Set the Froude number for free surface problems. More...
 
void SetTke_FreeStream (su2double val_tke_freestream)
 Set the Froude number for free surface problems. More...
 
void SetOmega_FreeStream (su2double val_omega_freestream)
 Set the Froude number for free surface problems. More...
 
void SetEnergy_FreeStreamND (su2double val_energy_freestreamnd)
 Set the Froude number for free surface problems. More...
 
void SetEnergy_FreeStream (su2double val_energy_freestream)
 Set the Froude number for free surface problems. More...
 
void SetThermalDiffusivity_Solid (su2double val_thermal_diffusivity)
 Set the thermal diffusivity for solids. More...
 
void SetTotal_UnstTimeND (su2double val_total_unsttimend)
 Set the Froude number for free surface problems. More...
 
su2double GetAoA (void)
 Get the angle of attack of the body. This is the angle between a reference line on a lifting body (often the chord line of an airfoil) and the vector representing the relative motion between the lifting body and the fluid through which it is moving. More...
 
su2double GetAoA_Offset (void)
 Get the off set angle of attack of the body. The solution and the geometry file are able to modifity the angle of attack in the config file. More...
 
su2double GetAoS_Offset (void)
 Get the off set sideslip angle of the body. The solution and the geometry file are able to modifity the angle of attack in the config file. More...
 
su2double GetAoA_Sens (void)
 Get the functional sensitivity with respect to changes in the angle of attack. More...
 
void SetAoA (su2double val_AoA)
 Set the angle of attack. More...
 
void SetAoA_Offset (su2double val_AoA_offset)
 Set the off set angle of attack. More...
 
void SetAoS_Offset (su2double val_AoS_offset)
 Set the off set sideslip angle. More...
 
void SetAoA_Sens (su2double val_AoA_sens)
 Set the angle of attack. More...
 
void SetAoS (su2double val_AoS)
 Set the angle of attack. More...
 
su2double GetAoS (void)
 Get the angle of sideslip of the body. It relates to the rotation of the aircraft centerline from the relative wind. More...
 
su2double GetChargeCoeff (void)
 Get the charge coefficient that is used in the poissonal potential simulation. More...
 
unsigned short GetnMGLevels (void)
 Get the number of multigrid levels. More...
 
void SetMGLevels (unsigned short val_nMGLevels)
 Set the number of multigrid levels. More...
 
unsigned short GetFinestMesh (void)
 Get the index of the finest grid. More...
 
unsigned short GetMGCycle (void)
 Get the kind of multigrid (V or W). More...
 
unsigned short GetGeometryMode (void)
 Get the king of evaluation in the geometrical module. More...
 
su2double GetCFL (unsigned short val_mesh)
 Get the Courant Friedrich Levi number for each grid. More...
 
su2double GetCFL_Solid (void)
 Get the Courant Friedrich Levi number for solid solvers. More...
 
void SetCFL (unsigned short val_mesh, su2double val_cfl)
 Get the Courant Friedrich Levi number for each grid. More...
 
su2double GetUnst_CFL (void)
 Get the Courant Friedrich Levi number for unsteady simulations. More...
 
bool GetReorientElements (void)
 Get information about element reorientation. More...
 
su2double GetMax_DeltaTime (void)
 Get the Courant Friedrich Levi number for unsteady simulations. More...
 
su2double GetParamDV (unsigned short val_dv, unsigned short val_param)
 Get a parameter of the particular design variable. More...
 
su2double GetCoordFFDBox (unsigned short val_ffd, unsigned short val_index)
 Get the coordinates of the FFD corner points. More...
 
unsigned short GetDegreeFFDBox (unsigned short val_ffd, unsigned short val_index)
 Get the degree of the FFD corner points. More...
 
string GetFFDTag (unsigned short val_dv)
 Get the FFD Tag of a particular design variable. More...
 
string GetTagFFDBox (unsigned short val_ffd)
 Get the FFD Tag of a particular FFD box. More...
 
unsigned short GetnDV (void)
 Get the number of design variables. More...
 
unsigned short GetnDV_Value (unsigned short iDV)
 Get the number of design variables. More...
 
unsigned short GetnFFDBox (void)
 Get the number of FFD boxes. More...
 
unsigned short GetFFD_Continuity (void)
 Get the required continuity level at the surface intersection with the FFD. More...
 
unsigned short GetFFD_CoordSystem (void)
 Get the coordinate system that we are going to use to define the FFD. More...
 
unsigned short GetFFD_Blending (void)
 Get the kind of FFD Blending function. More...
 
su2doubleGetFFD_BSplineOrder ()
 Get the kind BSpline Order in i,j,k direction. More...
 
unsigned short GetnRKStep (void)
 Get the number of Runge-Kutta steps. More...
 
unsigned short GetnLevels_TimeAccurateLTS (void)
 Get the number of time levels for time accurate local time stepping. More...
 
void SetnLevels_TimeAccurateLTS (unsigned short val_nLevels)
 Set the number of time levels for time accurate local time stepping. More...
 
unsigned short GetnTimeDOFsADER_DG (void)
 Get the number time DOFs for ADER-DG. More...
 
su2doubleGetTimeDOFsADER_DG (void)
 Get the location of the time DOFs for ADER-DG on the interval [-1..1]. More...
 
unsigned short GetnTimeIntegrationADER_DG (void)
 Get the number time integration points for ADER-DG. More...
 
su2doubleGetTimeIntegrationADER_DG (void)
 Get the location of the time integration points for ADER-DG on the interval [-1..1]. More...
 
su2doubleGetWeightsIntegrationADER_DG (void)
 Get the weights of the time integration points for ADER-DG. More...
 
unsigned short GetnMarker_All (void)
 Get the total number of boundary markers. More...
 
unsigned short GetnMarker_Max (void)
 Get the total number of boundary markers. More...
 
unsigned short GetnMarker_EngineInflow (void)
 Get the total number of boundary markers. More...
 
unsigned short GetnMarker_EngineExhaust (void)
 Get the total number of boundary markers. More...
 
unsigned short GetnMarker_NearFieldBound (void)
 Get the total number of boundary markers. More...
 
unsigned short GetnMarker_InterfaceBound (void)
 Get the total number of boundary markers. More...
 
unsigned short GetnMarker_Fluid_InterfaceBound (void)
 Get the total number of boundary markers. More...
 
unsigned short GetnMarker_Transpiration (void)
 Get the total number of transpiration markers. More...
 
unsigned short GetnMarker_ActDiskInlet (void)
 Get the total number of boundary markers. More...
 
unsigned short GetnMarker_ActDiskOutlet (void)
 Get the total number of boundary markers. More...
 
unsigned short GetnMarker_Monitoring (void)
 Get the total number of monitoring markers. More...
 
unsigned short GetnMarker_DV (void)
 Get the total number of DV markers. More...
 
unsigned short GetnMarker_Moving (void)
 Get the total number of moving markers. More...
 
unsigned short GetnMarker_PyCustom (void)
 Get the total number of Python customizable markers. More...
 
unsigned short GetnMarker_Analyze (void)
 Get the total number of moving markers. More...
 
unsigned short GetnMarker_Periodic (void)
 Get the total number of periodic markers. More...
 
unsigned short GetnMarker_HeatFlux (void)
 Get the total number of heat flux markers. More...
 
unsigned short GetnObj (void)
 Get the total number of objectives in kind_objective list. More...
 
void SetnMarker_All (unsigned short val_nmarker)
 Stores the number of marker in the simulation. More...
 
unsigned long GetnExtIter (void)
 Get the number of external iterations. More...
 
unsigned long GetUnst_nIntIter (void)
 Get the number of internal iterations. More...
 
unsigned long GetDyn_nIntIter (void)
 Get the number of internal iterations for the Newton-Raphson Method in nonlinear structural applications. More...
 
long GetUnst_RestartIter (void)
 Get the restart iteration number for unsteady simulations. More...
 
long GetUnst_AdjointIter (void)
 Get the starting direct iteration number for the unsteady adjoint (reverse time integration). More...
 
unsigned long GetIter_Avg_Objective (void)
 Number of iterations to average (reverse time integration). More...
 
long GetDyn_RestartIter (void)
 Get the restart iteration number for dynamic structural simulations. More...
 
unsigned short GetnTimeInstances (void)
 Retrieves the number of periodic time instances for Harmonic Balance. More...
 
su2double GetHarmonicBalance_Period (void)
 Retrieves the period of oscillations to be used with Harmonic Balance. More...
 
void SetnExtIter (unsigned long val_niter)
 Set the number of external iterations. More...
 
void SetExtIter (unsigned long val_iter)
 Set the current external iteration number. More...
 
void SetExtIter_OffSet (unsigned long val_iter)
 Set the current external iteration number. More...
 
void SetFSIIter (unsigned long val_iter)
 Set the current FSI iteration number. More...
 
void SetIntIter (unsigned long val_iter)
 Set the current internal iteration number. More...
 
unsigned long GetExtIter (void)
 Get the current external iteration number. More...
 
unsigned long GetExtIter_OffSet (void)
 Get the current internal iteration number. More...
 
unsigned long GetFSIIter (void)
 Get the current FSI iteration number. More...
 
unsigned long GetIntIter (void)
 Get the current internal iteration number. More...
 
unsigned long GetWrt_Sol_Freq (void)
 Get the frequency for writing the solution file. More...
 
unsigned long GetWrt_Sol_Freq_DualTime (void)
 Get the frequency for writing the solution file in Dual Time. More...
 
unsigned long GetWrt_Con_Freq (void)
 Get the frequency for writing the convergence file. More...
 
void SetWrt_Con_Freq (unsigned long val_freq)
 Set the frequency for writing the convergence file. More...
 
unsigned long GetWrt_Con_Freq_DualTime (void)
 Get the frequency for writing the convergence file in Dual Time. More...
 
bool GetWrt_Unsteady (void)
 Get information about writing unsteady headers and file extensions. More...
 
bool GetWrt_Output (void)
 Get information about writing output files. More...
 
bool GetWrt_Vol_Sol (void)
 Get information about writing a volume solution file. More...
 
bool GetLow_MemoryOutput (void)
 Get information about writing a volume solution file. More...
 
bool GetWrt_Srf_Sol (void)
 Get information about writing a surface solution file. More...
 
bool GetWrt_Csv_Sol (void)
 Get information about writing a surface comma-separated values (CSV) solution file. More...
 
bool GetWrt_Crd_Sol (void)
 Get information about writing a binary coordinates file. More...
 
bool GetWrt_Residuals (void)
 Get information about writing residuals to volume solution file. More...
 
bool GetWrt_Limiters (void)
 Get information about writing residuals to volume solution file. More...
 
bool GetWrt_Surface (void)
 Write solution at each surface. More...
 
bool GetWrt_SharpEdges (void)
 Get information about writing residuals to volume solution file. More...
 
bool GetWrt_Halo (void)
 Get information about writing rind layers to the solution files. More...
 
bool GetWrt_Performance (void)
 Get information about writing the performance summary at the end of a calculation. More...
 
bool GetWrt_InletFile (void)
 Get information about writing a template inlet profile file. More...
 
void SetWrt_InletFile (bool val_wrt_inletfile)
 Set information about writing a template inlet profile file. More...
 
bool GetWrt_Slice (void)
 Get information about writing a 1D slice of a 2D cartesian solution. More...
 
bool GetPlot_Section_Forces (void)
 Get information about writing sectional force files. More...
 
su2double Get_Alpha_RKStep (unsigned short val_step)
 Get the alpha (convective) coefficients for the Runge-Kutta integration scheme. More...
 
string GetMarker_All_TagBound (unsigned short val_marker)
 Get the index of the surface defined in the geometry file. More...
 
string GetMarker_ActDiskInlet_TagBound (unsigned short val_marker)
 Get the index of the surface defined in the geometry file. More...
 
string GetMarker_ActDiskOutlet_TagBound (unsigned short val_marker)
 Get the index of the surface defined in the geometry file. More...
 
string GetMarker_EngineInflow_TagBound (unsigned short val_marker)
 Get the index of the surface defined in the geometry file. More...
 
string GetMarker_EngineExhaust_TagBound (unsigned short val_marker)
 Get the index of the surface defined in the geometry file. More...
 
string GetMarker_Monitoring_TagBound (unsigned short val_marker)
 Get the name of the surface defined in the geometry file. More...
 
string GetMarker_HeatFlux_TagBound (unsigned short val_marker)
 Get the name of the surface defined in the geometry file. More...
 
short GetMarker_All_TagBound (string val_tag)
 Get the tag if the iMarker defined in the geometry file. More...
 
unsigned short GetMarker_All_KindBC (unsigned short val_marker)
 Get the kind of boundary for each marker. More...
 
void SetMarker_All_KindBC (unsigned short val_marker, unsigned short val_boundary)
 Set the value of the boundary val_boundary (read from the config file) for the marker val_marker. More...
 
void SetMarker_All_TagBound (unsigned short val_marker, string val_index)
 Set the value of the index val_index (read from the geometry file) for the marker val_marker. More...
 
void SetMarker_All_Monitoring (unsigned short val_marker, unsigned short val_monitoring)
 Set if a marker val_marker is going to be monitored val_monitoring (read from the config file). More...
 
void SetMarker_All_GeoEval (unsigned short val_marker, unsigned short val_geoeval)
 Set if a marker val_marker is going to be monitored val_monitoring (read from the config file). More...
 
void SetMarker_All_Designing (unsigned short val_marker, unsigned short val_designing)
 Set if a marker val_marker is going to be designed val_designing (read from the config file). More...
 
void SetMarker_All_Plotting (unsigned short val_marker, unsigned short val_plotting)
 Set if a marker val_marker is going to be plot val_plotting (read from the config file). More...
 
void SetMarker_All_Analyze (unsigned short val_marker, unsigned short val_analyze)
 Set if a marker val_marker is going to be plot val_plotting (read from the config file). More...
 
void SetMarker_All_ZoneInterface (unsigned short val_marker, unsigned short val_fsiinterface)
 Set if a marker val_marker is part of the FSI interface val_plotting (read from the config file). More...
 
void SetMarker_All_Turbomachinery (unsigned short val_marker, unsigned short val_turbo)
 Set if a marker val_marker is part of the Turbomachinery (read from the config file). More...
 
void SetMarker_All_TurbomachineryFlag (unsigned short val_marker, unsigned short val_turboflag)
 Set a flag to the marker val_marker part of the Turbomachinery (read from the config file). More...
 
void SetMarker_All_MixingPlaneInterface (unsigned short val_marker, unsigned short val_mixplan_interface)
 Set if a marker val_marker is part of the MixingPlane interface (read from the config file). More...
 
void SetMarker_All_DV (unsigned short val_marker, unsigned short val_DV)
 Set if a marker val_marker is going to be affected by design variables val_moving (read from the config file). More...
 
void SetMarker_All_Moving (unsigned short val_marker, unsigned short val_moving)
 Set if a marker val_marker is going to be moved val_moving (read from the config file). More...
 
void SetMarker_All_PyCustom (unsigned short val_marker, unsigned short val_PyCustom)
 Set if a marker val_marker is going to be customized in Python val_PyCustom (read from the config file). More...
 
void SetMarker_All_PerBound (unsigned short val_marker, short val_perbound)
 Set if a marker val_marker is going to be periodic val_perbound (read from the config file). More...
 
void SetMarker_All_SendRecv (unsigned short val_marker, short val_index)
 Set if a marker val_marker is going to be sent or receive val_index from another domain. More...
 
short GetMarker_All_SendRecv (unsigned short val_marker)
 Get the send-receive information for a marker val_marker. More...
 
short GetMarker_All_PerBound (unsigned short val_marker)
 Get an internal index that identify the periodic boundary conditions. More...
 
unsigned short GetMarker_All_Monitoring (unsigned short val_marker)
 Get the monitoring information for a marker val_marker. More...
 
unsigned short GetMarker_All_GeoEval (unsigned short val_marker)
 Get the monitoring information for a marker val_marker. More...
 
unsigned short GetMarker_All_Designing (unsigned short val_marker)
 Get the design information for a marker val_marker. More...
 
unsigned short GetMarker_All_Plotting (unsigned short val_marker)
 Get the plotting information for a marker val_marker. More...
 
unsigned short GetMarker_All_Analyze (unsigned short val_marker)
 Get the plotting information for a marker val_marker. More...
 
unsigned short GetMarker_All_ZoneInterface (unsigned short val_marker)
 Get the FSI interface information for a marker val_marker. More...
 
unsigned short GetMarker_All_MixingPlaneInterface (unsigned short val_marker)
 Get the MixingPlane interface information for a marker val_marker. More...
 
unsigned short GetMarker_All_Turbomachinery (unsigned short val_marker)
 Get the Turbomachinery information for a marker val_marker. More...
 
unsigned short GetMarker_All_TurbomachineryFlag (unsigned short val_marker)
 Get the Turbomachinery flag information for a marker val_marker. More...
 
unsigned short GetMarker_n_ZoneInterface (void)
 Get the number of FSI interface markers val_marker. More...
 
unsigned short GetMarker_All_DV (unsigned short val_marker)
 Get the DV information for a marker val_marker. More...
 
unsigned short GetMarker_All_Moving (unsigned short val_marker)
 Get the motion information for a marker val_marker. More...
 
unsigned short GetMarker_All_PyCustom (unsigned short val_marker)
 Get the Python customization for a marker val_marker. More...
 
su2double GetLocationStations (unsigned short val_section)
 Get the airfoil sections in the slicing process. More...
 
su2double GetNacelleLocation (unsigned short val_index)
 Get the defintion of the nacelle location. More...
 
unsigned short GetMG_PreSmooth (unsigned short val_mesh)
 Get the number of pre-smoothings in a multigrid strategy. More...
 
unsigned short GetMG_PostSmooth (unsigned short val_mesh)
 Get the number of post-smoothings in a multigrid strategy. More...
 
unsigned short GetMG_CorrecSmooth (unsigned short val_mesh)
 Get the number of implicit Jacobi smoothings of the correction in a multigrid strategy. More...
 
short GetFFD_Fix_IDir (unsigned short val_index)
 plane of the FFD (I axis) that should be fixed. More...
 
short GetFFD_Fix_JDir (unsigned short val_index)
 plane of the FFD (J axis) that should be fixed. More...
 
short GetFFD_Fix_KDir (unsigned short val_index)
 plane of the FFD (K axis) that should be fixed. More...
 
unsigned short GetnFFD_Fix_IDir (void)
 Get the number of planes to fix in the I direction. More...
 
unsigned short GetnFFD_Fix_JDir (void)
 Get the number of planes to fix in the J direction. More...
 
unsigned short GetnFFD_Fix_KDir (void)
 Get the number of planes to fix in the K direction. More...
 
unsigned short GetKind_Solver (void)
 Governing equations of the flow (it can be different from the run time equation). More...
 
void SetKind_Solver (unsigned short val_solver)
 Governing equations of the flow (it can be different from the run time equation). More...
 
unsigned short GetKind_Regime (void)
 Governing equations of the flow (it can be different from the run time equation). More...
 
unsigned short GetSystemMeasurements (void)
 Governing equations of the flow (it can be different from the run time equation). More...
 
unsigned short GetKind_GasModel (void)
 Gas model that we are using. More...
 
unsigned short GetKind_FluidModel (void)
 Fluid model that we are using. More...
 
unsigned short GetKind_DensityModel (void)
 Option to define the density model for incompressible flows. More...
 
bool GetEnergy_Equation (void)
 Flag for whether to solve the energy equation for incompressible flows. More...
 
unsigned short GetKind_FreeStreamOption (void)
 free stream option to initialize the solution More...
 
unsigned short GetKind_InitOption (void)
 free stream option to initialize the solution More...
 
su2double GetPressure_Critical (void)
 Get the value of the critical pressure. More...
 
su2double GetTemperature_Critical (void)
 Get the value of the critical temperature. More...
 
su2double GetAcentric_Factor (void)
 Get the value of the critical pressure. More...
 
unsigned short GetKind_ViscosityModel (void)
 Get the value of the viscosity model. More...
 
unsigned short GetKind_ConductivityModel (void)
 Get the value of the thermal conductivity model. More...
 
su2double GetMu_Constant (void)
 Get the value of the constant viscosity. More...
 
su2double GetMu_ConstantND (void)
 Get the value of the non-dimensional constant viscosity. More...
 
su2double GetKt_Constant (void)
 Get the value of the thermal conductivity. More...
 
su2double GetKt_ConstantND (void)
 Get the value of the non-dimensional thermal conductivity. More...
 
su2double GetMu_Ref (void)
 Get the value of the reference viscosity for Sutherland model. More...
 
su2double GetMu_RefND (void)
 Get the value of the non-dimensional reference viscosity for Sutherland model. More...
 
su2double GetMu_Temperature_Ref (void)
 Get the value of the reference temperature for Sutherland model. More...
 
su2double GetMu_Temperature_RefND (void)
 Get the value of the non-dimensional reference temperature for Sutherland model. More...
 
su2double GetMu_S (void)
 Get the value of the reference S for Sutherland model. More...
 
su2double GetMu_SND (void)
 Get the value of the non-dimensional reference S for Sutherland model. More...
 
void SetMu_ConstantND (su2double mu_const)
 Set the value of the non-dimensional constant viscosity. More...
 
void SetKt_ConstantND (su2double kt_const)
 Set the value of the non-dimensional thermal conductivity. More...
 
void SetMu_RefND (su2double mu_ref)
 Set the value of the non-dimensional reference viscosity for Sutherland model. More...
 
void SetMu_Temperature_RefND (su2double mu_Tref)
 Set the value of the non-dimensional reference temperature for Sutherland model. More...
 
void SetMu_SND (su2double mu_s)
 Set the value of the non-dimensional S for Sutherland model. More...
 
unsigned short GetKind_Gradient_Method (void)
 Get the kind of method for computation of spatial gradients. More...
 
unsigned short GetKind_Linear_Solver (void)
 Get the kind of solver for the implicit solver. More...
 
unsigned short GetKind_Linear_Solver_Prec (void)
 Get the kind of preconditioner for the implicit solver. More...
 
unsigned short GetKind_Deform_Linear_Solver (void)
 Get the kind of solver for the implicit solver. More...
 
void SetKind_Deform_Linear_Solver_Prec (unsigned short val_kind_prec)
 Set the kind of preconditioner for the implicit solver. More...
 
void SetKind_Linear_Solver_Prec (unsigned short val_kind_prec)
 Set the kind of preconditioner for the implicit solver. More...
 
su2double GetLinear_Solver_Error (void)
 Get min error of the linear solver for the implicit formulation. More...
 
su2double GetDeform_Linear_Solver_Error (void)
 Get min error of the linear solver for the implicit formulation. More...
 
unsigned long GetLinear_Solver_Iter (void)
 Get max number of iterations of the linear solver for the implicit formulation. More...
 
unsigned long GetDeform_Linear_Solver_Iter (void)
 Get max number of iterations of the linear solver for the implicit formulation. More...
 
unsigned short GetLinear_Solver_ILU_n (void)
 Get the ILU fill-in level for the linear solver. More...
 
unsigned long GetLinear_Solver_Restart_Frequency (void)
 Get restart frequency of the linear solver for the implicit formulation. More...
 
su2double GetRelaxation_Factor_Flow (void)
 Get the relaxation coefficient of the linear solver for the implicit formulation. More...
 
su2double GetRelaxation_Factor_AdjFlow (void)
 Get the relaxation coefficient of the linear solver for the implicit formulation. More...
 
su2double GetRelaxation_Factor_Turb (void)
 Get the relaxation coefficient of the linear solver for the implicit formulation. More...
 
su2double GetRelaxation_Factor_CHT (void)
 Get the relaxation coefficient of the CHT coupling. More...
 
su2double GetRoe_Kappa (void)
 Get the relaxation coefficient of the linear solver for the implicit formulation. More...
 
su2double GetSemiSpan (void)
 Get the wing semi span. More...
 
unsigned short GetKind_AdjTurb_Linear_Solver (void)
 Get the kind of solver for the implicit solver. More...
 
unsigned short GetKind_AdjTurb_Linear_Prec (void)
 Get the kind of preconditioner for the implicit solver. More...
 
unsigned short GetKind_DiscAdj_Linear_Solver (void)
 Get the kind of solver for the implicit solver. More...
 
unsigned short GetKind_DiscAdj_Linear_Prec (void)
 Get the kind of preconditioner for the implicit solver. More...
 
unsigned short GetKind_Deform_Linear_Solver_Prec (void)
 Get the kind of preconditioner for the implicit solver. More...
 
void SetKind_AdjTurb_Linear_Prec (unsigned short val_kind_prec)
 Set the kind of preconditioner for the implicit solver. More...
 
su2double GetAdjTurb_Linear_Error (void)
 Get min error of the linear solver for the implicit formulation. More...
 
su2double GetEntropyFix_Coeff (void)
 Get the entropy fix. More...
 
unsigned short GetAdjTurb_Linear_Iter (void)
 Get max number of iterations of the linear solver for the implicit formulation. More...
 
su2double GetCFLRedCoeff_AdjTurb (void)
 Get CFL reduction factor for adjoint turbulence model. More...
 
unsigned long GetGridDef_Linear_Iter (void)
 Get the number of linear smoothing iterations for mesh deformation. More...
 
unsigned long GetGridDef_Nonlinear_Iter (void)
 Get the number of nonlinear increments for mesh deformation. More...
 
bool GetDeform_Output (void)
 Get information about writing grid deformation residuals to the console. More...
 
su2double GetDeform_Tol_Factor (void)
 Get factor to multiply smallest volume for deform tolerance. More...
 
su2double GetDeform_Coeff (void)
 Get factor to multiply smallest volume for deform tolerance. More...
 
su2double GetDeform_Limit (void)
 Get limit for the volumetric deformation. More...
 
su2double GetDeform_ElasticityMod (void)
 Get Young's modulus for deformation (constant stiffness deformation) More...
 
su2double GetDeform_PoissonRatio (void)
 Get Poisson's ratio for deformation (constant stiffness deformation) . More...
 
unsigned short GetDeform_Stiffness_Type (void)
 Get the type of stiffness to impose for FEA mesh deformation. More...
 
bool GetVisualize_Volume_Def (void)
 Creates a tecplot file to visualize the volume deformation deformation made by the DEF software. More...
 
bool GetVisualize_Surface_Def (void)
 Creates a teot file to visualize the surface deformation deformation made by the DEF software. More...
 
bool GetFFD_Symmetry_Plane (void)
 Define the FFD box with a symetry plane. More...
 
unsigned short GetKind_SU2 (void)
 Get the kind of SU2 software component. More...
 
unsigned short GetRef_NonDim (void)
 Get the kind of non-dimensionalization. More...
 
unsigned short GetRef_Inc_NonDim (void)
 Get the kind of incompressible non-dimensionalization. More...
 
void SetKind_SU2 (unsigned short val_kind_su2)
 Get the kind of SU2 software component. More...
 
unsigned short GetKind_Turb_Model (void)
 Get the kind of the turbulence model. More...
 
unsigned short GetKind_Trans_Model (void)
 Get the kind of the transition model. More...
 
unsigned short GetKind_SGS_Model (void)
 Get the kind of the subgrid scale model. More...
 
unsigned short GetKind_Adaptation (void)
 Get the kind of adaptation technique. More...
 
su2double GetNew_Elem_Adapt (void)
 Get the number of new elements added in the adaptation process. More...
 
unsigned short GetKind_TimeIntScheme (void)
 Get the kind of time integration method. More...
 
unsigned short GetKind_ConvNumScheme (void)
 Get the kind of convective numerical scheme. More...
 
unsigned short GetKind_Centered (void)
 Get kind of center scheme for the convective terms. More...
 
unsigned short GetKind_Upwind (void)
 Get kind of upwind scheme for the convective terms. More...
 
bool GetMUSCL (void)
 Get if the upwind scheme used MUSCL or not. More...
 
bool GetMUSCL_Flow (void)
 Get if the upwind scheme used MUSCL or not. More...
 
bool GetMUSCL_Heat (void)
 Get if the upwind scheme used MUSCL or not. More...
 
bool GetMUSCL_Turb (void)
 Get if the upwind scheme used MUSCL or not. More...
 
bool GetMUSCL_AdjFlow (void)
 Get if the upwind scheme used MUSCL or not. More...
 
bool GetMUSCL_AdjTurb (void)
 Get if the upwind scheme used MUSCL or not. More...
 
unsigned short GetKind_TimeIntScheme_Flow (void)
 Get the kind of integration scheme (explicit or implicit) for the flow equations. More...
 
unsigned short GetKind_ADER_Predictor (void)
 Get the kind of scheme (aliased or non-aliased) to be used in the predictor step of ADER-DG. More...
 
unsigned short GetKind_TimeIntScheme_Heat (void)
 Get the kind of integration scheme (explicit or implicit) for the flow equations. More...
 
unsigned short GetKind_TimeStep_Heat (void)
 Get the kind of time stepping for the heat equation. More...
 
unsigned short GetKind_TimeIntScheme_FEA (void)
 Get the kind of integration scheme (explicit or implicit) for the flow equations. More...
 
unsigned short GetKind_TimeIntScheme_Template (void)
 Get the kind of integration scheme (explicit or implicit) for the template equations. More...
 
unsigned short GetKind_SpaceIteScheme_FEA (void)
 Get the kind of integration scheme (explicit or implicit) for the flow equations. More...
 
unsigned short GetKind_TransferMethod (void)
 Get the kind of transfer method we want to use for multiphysics problems. More...
 
unsigned short GetKind_ConvNumScheme_Flow (void)
 Get the kind of convective numerical scheme for the flow equations (centered or upwind). More...
 
unsigned short GetKind_ConvNumScheme_FEM_Flow (void)
 Get the kind of convective numerical scheme for the flow equations (finite element). More...
 
unsigned short GetKind_ConvNumScheme_Template (void)
 Get the kind of convective numerical scheme for the template equations (centered or upwind). More...
 
unsigned short GetKind_Centered_Flow (void)
 Get the kind of center convective numerical scheme for the flow equations. More...
 
unsigned short GetKind_Centered_Template (void)
 Get the kind of center convective numerical scheme for the plasma equations. More...
 
unsigned short GetKind_Upwind_Flow (void)
 Get the kind of upwind convective numerical scheme for the flow equations. More...
 
unsigned short GetKind_FEM_Flow (void)
 Get the kind of finite element convective numerical scheme for the flow equations. More...
 
unsigned short GetKind_FEM_DG_Shock (void)
 Get the kind of shock capturing method in FEM DG solver. More...
 
unsigned short GetKind_Matrix_Coloring (void)
 Get the kind of matrix coloring used for the sparse Jacobian computation. More...
 
unsigned short GetKind_SlopeLimit (void)
 Get the method for limiting the spatial gradients. More...
 
unsigned short GetKind_SlopeLimit_Flow (void)
 Get the method for limiting the spatial gradients. More...
 
unsigned short GetKind_SlopeLimit_Turb (void)
 Get the method for limiting the spatial gradients. More...
 
unsigned short GetKind_SlopeLimit_AdjTurb (void)
 Get the method for limiting the spatial gradients. More...
 
unsigned short GetKind_SlopeLimit_AdjFlow (void)
 Get the method for limiting the spatial gradients. More...
 
su2double GetKappa_1st_Flow (void)
 Value of the calibrated constant for the Lax method (center scheme). More...
 
su2double GetKappa_2nd_Flow (void)
 Value of the calibrated constant for the JST method (center scheme). More...
 
su2double GetKappa_4th_Flow (void)
 Value of the calibrated constant for the JST method (center scheme). More...
 
su2double GetKappa_2nd_Heat (void)
 Value of the calibrated constant for the JST method (center scheme). More...
 
su2double GetKappa_4th_Heat (void)
 Value of the calibrated constant for the JST-like method (center scheme). More...
 
unsigned short GetKind_TimeIntScheme_AdjFlow (void)
 Get the kind of integration scheme (explicit or implicit) for the adjoint flow equations. More...
 
unsigned short GetKind_ConvNumScheme_AdjFlow (void)
 Get the kind of convective numerical scheme for the adjoint flow equations (centered or upwind). More...
 
unsigned short GetKind_Centered_AdjFlow (void)
 Get the kind of center convective numerical scheme for the adjoint flow equations. More...
 
unsigned short GetKind_Upwind_AdjFlow (void)
 Get the kind of upwind convective numerical scheme for the adjoint flow equations. More...
 
su2double GetKappa_2nd_AdjFlow (void)
 Value of the calibrated constant for the high order method (center scheme). More...
 
su2double GetKappa_4th_AdjFlow (void)
 Value of the calibrated constant for the high order method (center scheme). More...
 
su2double GetKappa_1st_AdjFlow (void)
 Value of the calibrated constant for the low order method (center scheme). More...
 
unsigned short GetKind_TimeIntScheme_Turb (void)
 Get the kind of integration scheme (implicit) for the turbulence equations. More...
 
unsigned short GetKind_ConvNumScheme_Turb (void)
 Get the kind of convective numerical scheme for the turbulence equations (upwind). More...
 
unsigned short GetKind_Centered_Turb (void)
 Get the kind of center convective numerical scheme for the turbulence equations. More...
 
unsigned short GetKind_Upwind_Turb (void)
 Get the kind of upwind convective numerical scheme for the turbulence equations. More...
 
unsigned short GetKind_TimeIntScheme_AdjTurb (void)
 Get the kind of integration scheme (explicit or implicit) for the adjoint turbulence equations. More...
 
unsigned short GetKind_ConvNumScheme_AdjTurb (void)
 Get the kind of convective numerical scheme for the adjoint turbulence equations (centered or upwind). More...
 
unsigned short GetKind_ConvNumScheme_Heat (void)
 Get the kind of convective numerical scheme for the heat equation. More...
 
unsigned short GetKind_Centered_AdjTurb (void)
 Get the kind of center convective numerical scheme for the adjoint turbulence equations. More...
 
unsigned short GetKind_Upwind_AdjTurb (void)
 Get the kind of upwind convective numerical scheme for the adjoint turbulence equations. More...
 
bool GetFrozen_Visc_Cont (void)
 Provides information about the way in which the turbulence will be treated by the cont. adjoint method. More...
 
bool GetFrozen_Visc_Disc (void)
 Provides information about the way in which the turbulence will be treated by the disc. adjoint method. More...
 
bool GetInconsistent_Disc (void)
 Provides information about using an inconsistent (primal/dual) discrete adjoint formulation. More...
 
bool GetFrozen_Limiter_Disc (void)
 Provides information about the way in which the limiter will be treated by the disc. adjoint method. More...
 
bool GetWrite_Conv_FSI (void)
 Write convergence file for FSI problems. More...
 
bool GetSens_Remove_Sharp (void)
 Provides information about if the sharp edges are going to be removed from the sensitivity. More...
 
unsigned short GetKind_Inlet (void)
 Get the kind of inlet boundary condition treatment (total conditions or mass flow). More...
 
bool GetInlet_Profile_From_File (void)
 Check if the inlet profile(s) are specified in an input file. More...
 
string GetInlet_FileName (void)
 Get name of the input file for the specified inlet profile. More...
 
su2double GetInlet_Profile_Matching_Tolerance (void)
 Get the tolerance used for matching two points on a specified inlet. More...
 
unsigned short GetKind_Inc_Inlet (string val_marker)
 Get the type of incompressible inlet from the list. More...
 
unsigned short GetnInc_Inlet (void)
 Get the total number of types in Kind_Inc_Inlet list. More...
 
bool GetInc_Inlet_UseNormal (void)
 Flag for whether the local boundary normal is used as the flow direction for an incompressible pressure inlet. More...
 
unsigned short GetKind_AverageProcess (void)
 Get the kind of mixing process for averaging quantities at the boundaries. More...
 
unsigned short GetKind_PerformanceAverageProcess (void)
 Get the kind of mixing process for averaging quantities at the boundaries. More...
 
void SetKind_AverageProcess (unsigned short new_AverageProcess)
 Set the kind of mixing process for averaging quantities at the boundaries. More...
 
void SetKind_PerformanceAverageProcess (unsigned short new_AverageProcess)
 Set the kind of mixing process for averaging quantities at the boundaries. More...
 
su2double GetRampRotatingFrame_Coeff (unsigned short iCoeff)
 Get coeff for Rotating Frame Ramp. More...
 
bool GetRampRotatingFrame (void)
 Get Rotating Frame Ramp option. More...
 
su2double GetRampOutletPressure_Coeff (unsigned short iCoeff)
 Get coeff for Outlet Pressure Ramp. More...
 
su2double GetFinalOutletPressure (void)
 Get final Outlet Pressure value for the ramp. More...
 
su2double GetMonitorOutletPressure (void)
 Get final Outlet Pressure value for the ramp. More...
 
void SetMonitotOutletPressure (su2double newMonPres)
 Set Monitor Outlet Pressure value for the ramp. More...
 
bool GetRampOutletPressure (void)
 Get Outlet Pressure Ramp option. More...
 
su2double GetMixedout_Coeff (unsigned short iCoeff)
 Get mixedout coefficients. More...
 
su2double GetExtraRelFacGiles (unsigned short iCoeff)
 Get extra relaxation factor coefficients for the Giels BC. More...
 
su2double GetAverageMachLimit (void)
 Get mach limit for average massflow-based procedure . More...
 
unsigned short GetKind_MixingPlaneInterface (void)
 Get the kind of mixing process for averaging quantities at the boundaries. More...
 
unsigned short GetKind_TurboMachinery (unsigned short val_iZone)
 Get the kind of turbomachinery architecture. More...
 
unsigned short GetKind_SpanWise (void)
 Get the kind of turbomachinery architecture. More...
 
bool GetBoolMixingPlaneInterface (void)
 Verify if there is mixing plane interface specified from config file. More...
 
bool GetBoolTurbMixingPlane (void)
 Verify if there is mixing plane interface specified from config file. More...
 
bool GetSpatialFourier (void)
 Verify if there is mixing plane interface specified from config file. More...
 
unsigned short GetnMarker_MixingPlaneInterface (void)
 number mixing plane interface specified from config file. More...
 
bool GetBoolTurbomachinery (void)
 Verify if there is Turbomachinery performance option specified from config file. More...
 
bool GetBoolZoneSpecific (void)
 Verify if there are zone specific solvers entered in the config file. More...
 
su2double GetnBlades (unsigned short val_iZone)
 number Turbomachinery blades computed using the pitch information. More...
 
void SetnBlades (unsigned short val_iZone, su2double nblades)
 number Turbomachinery blades computed using the pitch information. More...
 
bool GetBoolGiles (void)
 Verify if there is any Giles Boundary Condition option specified from config file. More...
 
bool GetBoolRiemann (void)
 Verify if there is any Riemann Boundary Condition option specified from config file. More...
 
unsigned short GetnMarker_Turbomachinery (void)
 number Turbomachinery performance option specified from config file. More...
 
unsigned short GetnMarker_Shroud (void)
 Get number of shroud markers. More...
 
string GetMarker_Shroud (unsigned short val_marker)
 Get the marker shroud. More...
 
unsigned short GetnMarker_TurboPerformance (void)
 number Turbomachinery performance option specified from config file. More...
 
unsigned short Get_nSpanWiseSections_User (void)
 number span-wise sections to compute 3D BC and performance for turbomachinery specified by the user. More...
 
unsigned short GetnSpanWiseSections (void)
 number span-wise sections to compute 3D BC and performance for turbomachinery. More...
 
void SetnSpanMaxAllZones (unsigned short val_nSpna_max)
 set number of maximum span-wise sections among all zones . More...
 
unsigned short GetnSpanMaxAllZones (void)
 number span-wise sections to compute performance for turbomachinery. More...
 
void SetnSpanWiseSections (unsigned short nSpan)
 set number span-wise sections to compute 3D BC and performance for turbomachinery. More...
 
unsigned short GetnSpan_iZones (unsigned short iZone)
 set number span-wise sections to compute 3D BC and performance for turbomachinery. More...
 
void SetnSpan_iZones (unsigned short nSpan, unsigned short iZone)
 set number span-wise sections to compute 3D BC and performance for turbomachinery. More...
 
string GetMarker_TurboPerf_BoundIn (unsigned short index)
 get inlet bounds name for Turbomachinery performance calculation. More...
 
string GetMarker_TurboPerf_BoundOut (unsigned short index)
 get outlet bounds name for Turbomachinery performance calculation. More...
 
unsigned short GetKind_TurboPerf (unsigned short index)
 get marker kind for Turbomachinery performance calculation. More...
 
string GetMarker_PerBound (unsigned short val_marker)
 get outlet bounds name for Turbomachinery performance calculation. More...
 
unsigned short GetKind_Engine_Inflow (void)
 Get the kind of inlet boundary condition treatment (total conditions or mass flow). More...
 
unsigned short GetKind_ActDisk (void)
 Get the kind of inlet boundary condition treatment (total conditions or mass flow). More...
 
unsigned short GetnLocationStations (void)
 Get the number of sections. More...
 
unsigned short GetnWingStations (void)
 Get the number of sections for computing internal volume. More...
 
su2double GetGeo_Waterline_Location (void)
 Get the location of the waterline. More...
 
bool GetHold_GridFixed (void)
 Provides information about the the nodes that are going to be moved on a deformation volumetric grid deformation. More...
 
unsigned short GetKind_ObjFunc (void)
 Get the kind of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc. More...
 
unsigned short GetKind_ObjFunc (unsigned short val_obj)
 Get the kind of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc. More...
 
su2double GetWeight_ObjFunc (unsigned short val_obj)
 Get the weight of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc. More...
 
void SetWeight_ObjFunc (unsigned short val_obj, su2double val)
 Set the weight of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc. More...
 
su2double GetCoeff_ObjChainRule (unsigned short iVar)
 Get the coefficients of the objective defined by the chain rule with primitive variables. More...
 
bool GetComboObj (void)
 Get the flag indicating whether to comput a combined objective. More...
 
unsigned short GetKind_SensSmooth (void)
 Get the kind of sensitivity smoothing technique. More...
 
unsigned short GetUnsteady_Simulation (void)
 Provides information about the time integration, and change the write in the output files information about the iteration. More...
 
unsigned short GetnReactions (void)
 Provides the number of chemical reactions in the chemistry model. More...
 
su2double GetArrheniusCoeff (unsigned short iReaction)
 Provides the number of chemical reactions in the chemistry model. More...
 
su2double GetArrheniusEta (unsigned short iReaction)
 Provides the number of chemical reactions in the chemistry model. More...
 
su2double GetArrheniusTheta (unsigned short iReaction)
 Provides the number of chemical reactions in the chemistry model. More...
 
su2doubleGetRxnTcf_a (void)
 Provides the rate controlling temperature exponents for chemistry. More...
 
su2doubleGetRxnTcf_b (void)
 Provides the rate controlling temperature exponents for chemistry. More...
 
su2doubleGetRxnTcb_a (void)
 Provides the rate controlling temperature exponents for chemistry. More...
 
su2doubleGetRxnTcb_b (void)
 Provides the rate controlling temperature exponents for chemistry. More...
 
su2doubleGetDissociationPot (void)
 Dissociation potential of species. More...
 
su2doubleGetRotationModes (void)
 Provides the number of rotational modes of energy storage. More...
 
su2doubleGetCharVibTemp (void)
 Provides the characteristic vibrational temperature for calculating e_vib. More...
 
su2double ** GetCharElTemp (void)
 Provides the characteristic electronic temperature for calculating e_el. More...
 
su2double ** GetElDegeneracy (void)
 Provides the degeneracy of electron states for calculating e_el. More...
 
unsigned short * GetnElStates (void)
 Provides number electron states for calculating e_el. More...
 
su2doubleGetRefTemperature (void)
 Provides the thermodynamic reference temperatures from the JANAF tables. More...
 
su2double GetCharVibTemp (unsigned short iSpecies)
 Provides the characteristic vibrational temperature for calculating e_vib. More...
 
su2doubleGetMolar_Mass (void)
 Provides the molar mass of each species present in multi species fluid. More...
 
su2double GetMolar_Mass (unsigned short iSpecies)
 Provides the molar mass of each species present in multi species fluid. More...
 
unsigned short GetnMonatomics (void)
 Retrieves the number of monatomic species in the multicomponent gas. More...
 
unsigned short GetnDiatomics (void)
 Retrieves the number of monatomic species in the multicomponent gas. More...
 
su2double GetInitial_Gas_Composition (unsigned short iSpecies)
 Provides the molar mass of each species present in multi species fluid. More...
 
su2doubleGetEnthalpy_Formation (void)
 Provides the formation enthalpy of the specified species at standard conditions. More...
 
su2double GetEnthalpy_Formation (unsigned short iSpecies)
 Provides the formation enthalpy of the specified species at standard conditions. More...
 
bool GetRestart (void)
 Provides the restart information. More...
 
bool GetWrt_Binary_Restart (void)
 Flag for whether binary SU2 native restart files are written. More...
 
bool GetRead_Binary_Restart (void)
 Flag for whether binary SU2 native restart files are read. More...
 
unsigned short GetnVar (void)
 Provides the number of varaibles. More...
 
unsigned short GetnZone (void)
 Provides the number of varaibles. More...
 
unsigned short GetiZone (void)
 Provides the number of varaibles. More...
 
bool GetRestart_Flow (void)
 For some problems like adjoint or the linearized equations it is necessary to restart the flow solution. More...
 
bool GetIonization (void)
 Indicates whether electron gas is present in the gas mixture. More...
 
bool GetEquivArea (void)
 Information about computing and plotting the equivalent area distribution. More...
 
bool GetInvDesign_Cp (void)
 Information about computing and plotting the equivalent area distribution. More...
 
bool GetInvDesign_HeatFlux (void)
 Information about computing and plotting the equivalent area distribution. More...
 
string GetMesh_FileName (void)
 Get name of the input grid. More...
 
string GetMesh_Out_FileName (void)
 Get name of the output grid, this parameter is important for grid adaptation and deformation. More...
 
string GetSolution_FlowFileName (void)
 Get the name of the file with the solution of the flow problem. More...
 
string GetSolution_AdjFileName (void)
 Get the name of the file with the solution of the adjoint flow problem with drag objective function. More...
 
string GetSolution_FEMFileName (void)
 Get the name of the file with the solution of the structural problem. More...
 
string GetSolution_AdjFEMFileName (void)
 Get the name of the file with the solution of the adjoint structural problem. More...
 
string GetResidual_FileName (void)
 Get the name of the file with the residual of the problem. More...
 
unsigned short GetMesh_FileFormat (void)
 Get the format of the input/output grid. More...
 
unsigned short GetOutput_FileFormat (void)
 Get the format of the output solution. More...
 
unsigned short GetActDisk_Jump (void)
 Get the format of the output solution. More...
 
string GetConv_FileName (void)
 Get the name of the file with the convergence history of the problem. More...
 
string GetConv_FileName_FSI (void)
 Get the name of the file with the convergence history of the problem for FSI applications. More...
 
string GetBreakdown_FileName (void)
 Get the name of the file with the forces breakdown of the problem. More...
 
string GetFlow_FileName (void)
 Get the name of the file with the flow variables. More...
 
string GetStructure_FileName (void)
 Get the name of the file with the structure variables. More...
 
string GetSurfStructure_FileName (void)
 Get the name of the file with the structure variables. More...
 
string GetAdjStructure_FileName (void)
 Get the name of the file with the adjoint structure variables. More...
 
string GetAdjSurfStructure_FileName (void)
 Get the name of the file with the adjoint structure variables. More...
 
string GetSurfHeat_FileName (void)
 Get the name of the file with the structure variables. More...
 
string GetHeat_FileName (void)
 Get the name of the file with the wave variables. More...
 
string GetRestart_HeatFileName (void)
 Get the name of the restart file for the heat variables. More...
 
string GetMultizone_FileName (string val_filename, int val_iZone)
 Append the zone index to the restart or the solution files. More...
 
string GetMultizone_HistoryFileName (string val_filename, int val_iZone)
 Append the zone index to the restart or the solution files. More...
 
string GetMultiInstance_FileName (string val_filename, int val_iInst)
 Append the instance index to the restart or the solution files. More...
 
string GetMultiInstance_HistoryFileName (string val_filename, int val_iInst)
 Append the instance index to the restart or the solution files. More...
 
string GetRestart_FlowFileName (void)
 Get the name of the restart file for the flow variables. More...
 
string GetRestart_AdjFileName (void)
 Get the name of the restart file for the adjoint variables (drag objective function). More...
 
string GetRestart_FEMFileName (void)
 Get the name of the restart file for the structural variables. More...
 
string GetRestart_AdjFEMFileName (void)
 Get the name of the restart file for the structural adjoint variables. More...
 
string GetAdj_FileName (void)
 Get the name of the file with the adjoint variables. More...
 
string GetObjFunc_Grad_FileName (void)
 Get the name of the file with the gradient of the objective function. More...
 
string GetObjFunc_Value_FileName (void)
 Get the name of the file with the gradient of the objective function. More...
 
string GetSurfFlowCoeff_FileName (void)
 Get the name of the file with the surface information for the flow problem. More...
 
string GetSurfAdjCoeff_FileName (void)
 Get the name of the file with the surface information for the adjoint problem. More...
 
string GetSurfSens_FileName (void)
 Get the name of the file with the surface sensitivity (discrete adjoint). More...
 
string GetVolSens_FileName (void)
 Get the name of the file with the volume sensitivity (discrete adjoint). More...
 
string GetUnsteady_FileName (string val_filename, int val_iter)
 Augment the input filename with the iteration number for an unsteady file. More...
 
string GetObjFunc_Extension (string val_filename)
 Append the input filename string with the appropriate objective function extension. More...
 
unsigned short GetResidual_Criteria_FEM (void)
 Get the criteria for structural residual (relative/absolute). More...
 
unsigned short GetResidual_Func_Flow (void)
 Get functional that is going to be used to evaluate the residual flow convergence. More...
 
unsigned short GetCauchy_Func_Flow (void)
 Get functional that is going to be used to evaluate the flow convergence. More...
 
unsigned short GetCauchy_Func_AdjFlow (void)
 Get functional that is going to be used to evaluate the adjoint flow convergence. More...
 
unsigned short GetCauchy_Elems (void)
 Get the number of iterations that are considered in the Cauchy convergence criteria. More...
 
unsigned long GetStartConv_Iter (void)
 Get the number of iterations that are not considered in the convergence criteria. More...
 
su2double GetCauchy_Eps (void)
 Get the value of convergence criteria for the Cauchy method in the direct, adjoint or linearized problem. More...
 
su2double GetDelta_UnstTimeND (void)
 If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation. More...
 
su2double GetTotal_UnstTimeND (void)
 If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation. More...
 
su2double GetDelta_UnstTime (void)
 If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation. More...
 
void SetDelta_UnstTimeND (su2double val_delta_unsttimend)
 Set the value of the unsteadty time step using the CFL number. More...
 
su2double GetTotal_UnstTime (void)
 If we are performing an unsteady simulation, this is the value of max physical time for which we run the simulation. More...
 
su2double GetCurrent_UnstTime (void)
 If we are performing an unsteady simulation, this is the value of current time. More...
 
bool GetSubsonicEngine (void)
 Divide the rectbles and hexahedron. More...
 
bool GetActDisk_DoubleSurface (void)
 Actuator disk defined with a double surface. More...
 
bool GetEngine_HalfModel (void)
 Only halg of the engine is in the compputational grid. More...
 
bool GetActDisk_SU2_DEF (void)
 Actuator disk defined with a double surface. More...
 
su2double GetDV_Value (unsigned short val_dv, unsigned short val_val=0)
 Value of the design variable step, we use this value in design problems. More...
 
void SetDV_Value (unsigned short val_dv, unsigned short val_ind, su2double val)
 Set the value of the design variable step, we use this value in design problems. More...
 
bool GetGrid_Movement (void)
 Get information about the grid movement. More...
 
unsigned short GetKind_GridMovement (unsigned short val_iZone)
 Get the type of dynamic mesh motion. More...
 
void SetKind_GridMovement (unsigned short val_iZone, unsigned short motion_Type)
 Set the type of dynamic mesh motion. More...
 
su2double GetMach_Motion (void)
 Get the mach number based on the mesh velocity and freestream quantities. More...
 
su2double GetMotion_Origin_X (unsigned short val_iZone)
 Get x-coordinate of the mesh motion origin. More...
 
su2double GetMotion_Origin_Y (unsigned short val_iZone)
 Get y-coordinate of the mesh motion origin. More...
 
su2double GetMotion_Origin_Z (unsigned short val_iZone)
 Get z-coordinate of the mesh motion origin. More...
 
void SetMotion_Origin_X (unsigned short val_iZone, su2double val_origin)
 Set x-coordinate of the mesh motion origin. More...
 
void SetMotion_Origin_Y (unsigned short val_iZone, su2double val_origin)
 Set y-coordinate of the mesh motion origin. More...
 
void SetMotion_Origin_Z (unsigned short val_iZone, su2double val_origin)
 Set z-coordinate of the mesh motion origin. More...
 
su2double GetTranslation_Rate_X (unsigned short val_iZone)
 Get the translational velocity of the mesh in the x-direction. More...
 
su2double GetTranslation_Rate_Y (unsigned short val_iZone)
 Get the translational velocity of the mesh in the y-direction. More...
 
su2double GetTranslation_Rate_Z (unsigned short val_iZone)
 Get the translational velocity of the mesh in the z-direction. More...
 
su2double GetRotation_Rate_X (unsigned short val_iZone)
 Get the angular velocity of the mesh about the x-axis. More...
 
su2double GetRotation_Rate_Y (unsigned short val_iZone)
 Get the angular velocity of the mesh about the y-axis. More...
 
su2double GetRotation_Rate_Z (unsigned short val_iZone)
 Get the angular velocity of the mesh about the z-axis. More...
 
su2double GetFinalRotation_Rate_Z (unsigned short val_iZone)
 Get the angular velocity of the mesh about the z-axis. More...
 
void SetRotation_Rate_Z (su2double newRotation_Rate_Z, unsigned short val_iZone)
 Set the angular velocity of the mesh about the z-axis. More...
 
su2double GetPitching_Omega_X (unsigned short val_iZone)
 Get the angular frequency of a mesh pitching about the x-axis. More...
 
su2double GetPitching_Omega_Y (unsigned short val_iZone)
 Get the angular frequency of a mesh pitching about the y-axis. More...
 
su2double GetPitching_Omega_Z (unsigned short val_iZone)
 Get the angular frequency of a mesh pitching about the z-axis. More...
 
su2double GetPitching_Ampl_X (unsigned short val_iZone)
 Get the pitching amplitude about the x-axis. More...
 
su2double GetPitching_Ampl_Y (unsigned short val_iZone)
 Get the pitching amplitude about the y-axis. More...
 
su2double GetPitching_Ampl_Z (unsigned short val_iZone)
 Get the pitching amplitude about the z-axis. More...
 
su2double GetPitching_Phase_X (unsigned short val_iZone)
 Get the pitching phase offset about the x-axis. More...
 
su2double GetPitching_Phase_Y (unsigned short val_iZone)
 Get the pitching phase offset about the y-axis. More...
 
su2double GetPitching_Phase_Z (unsigned short val_iZone)
 Get the pitching phase offset about the z-axis. More...
 
su2double GetPlunging_Omega_X (unsigned short val_iZone)
 Get the angular frequency of a mesh plunging in the x-direction. More...
 
su2double GetPlunging_Omega_Y (unsigned short val_iZone)
 Get the angular frequency of a mesh plunging in the y-direction. More...
 
su2double GetPlunging_Omega_Z (unsigned short val_iZone)
 Get the angular frequency of a mesh plunging in the z-direction. More...
 
su2double GetPlunging_Ampl_X (unsigned short val_iZone)
 Get the plunging amplitude in the x-direction. More...
 
su2double GetPlunging_Ampl_Y (unsigned short val_iZone)
 Get the plunging amplitude in the y-direction. More...
 
su2double GetPlunging_Ampl_Z (unsigned short val_iZone)
 Get the plunging amplitude in the z-direction. More...
 
su2doubleGetOmega_HB (void)
 Get the Harmonic Balance frequency pointer. More...
 
bool GetHB_Precondition (void)
 Get if harmonic balance source term is to be preconditioned. More...
 
unsigned short GetMoveMotion_Origin (unsigned short val_marker)
 Get if we should update the motion origin. More...
 
su2double GetminTurkelBeta ()
 Get the minimum value of Beta for Roe-Turkel preconditioner. More...
 
su2double GetmaxTurkelBeta ()
 Get the minimum value of Beta for Roe-Turkel preconditioner. More...
 
bool GetAdiabaticWall (void)
 Get information about the adibatic wall condition. More...
 
bool GetIsothermalWall (void)
 Get information about the isothermal wall condition. More...
 
bool Low_Mach_Preconditioning (void)
 Get information about the Low Mach Preconditioning. More...
 
bool Low_Mach_Correction (void)
 Get information about the Low Mach Correction. More...
 
bool GetPoissonSolver (void)
 Get information about the poisson solver condition. More...
 
bool GetGravityForce (void)
 Get information about the gravity force. More...
 
bool GetBody_Force (void)
 Get information about the body force. More...
 
su2doubleGetBody_Force_Vector (void)
 Get a pointer to the body force vector. More...
 
bool GetRotating_Frame (void)
 Get information about the rotational frame. More...
 
bool GetAxisymmetric (void)
 Get information about the axisymmetric frame. More...
 
bool GetDebugMode (void)
 Get information about the axisymmetric frame. More...
 
bool GetAdaptBoundary (void)
 Get information about there is a smoothing of the grid coordinates. More...
 
bool GetSmoothNumGrid (void)
 Get information about there is a smoothing of the grid coordinates. More...
 
void SetSmoothNumGrid (bool val_smoothnumgrid)
 Set information about there is a smoothing of the grid coordinates. More...
 
void SubtractFinestMesh (void)
 Subtract one to the index of the finest grid (full multigrid strategy). More...
 
unsigned short GetDesign_Variable (unsigned short val_dv)
 Obtain the kind of design variable. More...
 
string GetTranspTag (unsigned short val_dv)
 Obtain the marker of a transpiration DV. More...
 
bool GetTranspiration_Objective (void)
 Provides the transpiration objective information. More...
 
bool GetBuffet_Monitoring (void)
 Provides the buffet monitoring information. More...
 
su2double GetBuffet_k (void)
 Get the buffet sensor sharpness coefficient. More...
 
su2double GetBuffet_lambda (void)
 Get the buffet sensor offset parameter. More...
 
unsigned short GetConvCriteria (void)
 Obtain the kind of convergence criteria to establish the convergence of the CFD code. More...
 
unsigned short GetMarker_CfgFile_TagBound (string val_marker)
 Get the index in the config information of the marker val_marker. More...
 
string GetMarker_CfgFile_TagBound (unsigned short val_marker)
 Get the name in the config information of the marker number val_marker. More...
 
unsigned short GetMarker_CfgFile_KindBC (string val_marker)
 Get the boundary information (kind of boundary) in the config information of the marker val_marker. More...
 
unsigned short GetMarker_CfgFile_Monitoring (string val_marker)
 Get the monitoring information from the config definition for the marker val_marker. More...
 
unsigned short GetMarker_CfgFile_GeoEval (string val_marker)
 Get the monitoring information from the config definition for the marker val_marker. More...
 
unsigned short GetMarker_CfgFile_Designing (string val_marker)
 Get the monitoring information from the config definition for the marker val_marker. More...
 
unsigned short GetMarker_CfgFile_Plotting (string val_marker)
 Get the plotting information from the config definition for the marker val_marker. More...
 
unsigned short GetMarker_CfgFile_Analyze (string val_marker)
 Get the plotting information from the config definition for the marker val_marker. More...
 
unsigned short GetMarker_CfgFile_ZoneInterface (string val_marker)
 Get the FSI interface information from the config definition for the marker val_marker. More...
 
unsigned short GetMarker_CfgFile_Turbomachinery (string val_marker)
 Get the TurboPerformance information from the config definition for the marker val_marker. More...
 
unsigned short GetMarker_CfgFile_TurbomachineryFlag (string val_marker)
 Get the TurboPerformance flag information from the config definition for the marker val_marker. More...
 
unsigned short GetMarker_CfgFile_MixingPlaneInterface (string val_marker)
 Get the MixingPlane interface information from the config definition for the marker val_marker. More...
 
unsigned short GetMarker_CfgFile_DV (string val_marker)
 Get the DV information from the config definition for the marker val_marker. More...
 
unsigned short GetMarker_CfgFile_Moving (string val_marker)
 Get the motion information from the config definition for the marker val_marker. More...
 
unsigned short GetMarker_CfgFile_PyCustom (string val_marker)
 Get the Python customization information from the config definition for the marker val_marker. More...
 
unsigned short GetMarker_CfgFile_PerBound (string val_marker)
 Get the periodic information from the config definition of the marker val_marker. More...
 
int GetMarker_ZoneInterface (string val_marker)
 Get the name of the marker val_marker. More...
 
bool GetContinuous_Adjoint (void)
 Determines if problem is adjoint. More...
 
bool GetViscous (void)
 Determines if problem is viscous. More...
 
unsigned short GetContainerPosition (unsigned short val_eqsystem)
 Provides the index of the solution in the container. More...
 
su2double GetOrderMagResidual (void)
 Value of the order of magnitude reduction of the residual. More...
 
su2double GetMinLogResidual (void)
 Value of the minimum residual value (log10 scale). More...
 
su2double GetOrderMagResidualFSI (void)
 Value of the order of magnitude reduction of the residual for FSI applications. More...
 
su2double GetMinLogResidualFSI (void)
 Value of the minimum residual value for FSI applications (log10 scale). More...
 
su2double GetOrderMagResidual_BGS_F (void)
 Value of the order of magnitude reduction of the flow residual for BGS applications. More...
 
su2double GetMinLogResidual_BGS_F (void)
 Value of the minimum flow residual value for BGS applications (log10 scale). More...
 
su2double GetOrderMagResidual_BGS_S (void)
 Value of the order of magnitude reduction of the flow residual for BGS applications. More...
 
su2double GetMinLogResidual_BGS_S (void)
 Value of the minimum flow residual value for BGS applications (log10 scale). More...
 
su2double GetResidual_FEM_UTOL (void)
 Value of the displacement tolerance UTOL for FEM structural analysis (log10 scale). More...
 
su2double GetResidual_FEM_RTOL (void)
 Value of the displacement tolerance UTOL for FEM structural analysis (log10 scale). More...
 
su2double GetResidual_FEM_ETOL (void)
 Value of the displacement tolerance UTOL for FEM structural analysis (log10 scale). More...
 
su2double GetCriteria_FEM_ADJ (void)
 Value of the maximum objective function for FEM elasticity adjoint (log10 scale). More...
 
su2double GetDamp_Engine_Inflow (void)
 Value of the damping factor for the engine inlet bc. More...
 
su2double GetDamp_Engine_Exhaust (void)
 Value of the damping factor for the engine exhaust inlet bc. More...
 
su2double GetDamp_Res_Restric (void)
 Value of the damping factor for the residual restriction. More...
 
su2double GetDamp_Correc_Prolong (void)
 Value of the damping factor for the correction prolongation. More...
 
su2double GetPosition_Plane (void)
 Value of the position of the Near Field (y coordinate for 2D, and z coordinate for 3D). More...
 
su2double GetWeightCd (void)
 Value of the weight of the drag coefficient in the Sonic Boom optimization. More...
 
void SetdNetThrust_dBCThrust (su2double val_dnetthrust_dbcthrust)
 Value of the weight of the CD, CL, CM optimization. More...
 
su2double GetFixAzimuthalLine (void)
 Value of the azimuthal line to fix due to a misalignments of the nearfield. More...
 
su2double GetdCD_dCMy (void)
 Value of the weight of the CD, CL, CM optimization. More...
 
su2double GetCM_Target (void)
 Value of the weight of the CD, CL, CM optimization. More...
 
su2double GetdCD_dCL (void)
 Value of the weight of the CD, CL, CM optimization. More...
 
void SetdCD_dCL (su2double val_dcd_dcl)
 Value of the weight of the CD, CL, CM optimization. More...
 
su2double GetdCMx_dCL (void)
 Value of the weight of the CD, CL, CM optimization. More...
 
void SetdCMx_dCL (su2double val_dcmx_dcl)
 Value of the weight of the CD, CL, CM optimization. More...
 
su2double GetdCMy_dCL (void)
 Value of the weight of the CD, CL, CM optimization. More...
 
void SetdCMy_dCL (su2double val_dcmy_dcl)
 Value of the weight of the CD, CL, CM optimization. More...
 
su2double GetdCMz_dCL (void)
 Value of the weight of the CD, CL, CM optimization. More...
 
void SetdCMz_dCL (su2double val_dcmz_dcl)
 Value of the weight of the CD, CL, CM optimization. More...
 
void SetdCL_dAlpha (su2double val_dcl_dalpha)
 Value of the weight of the CD, CL, CM optimization. More...
 
void SetdCM_diH (su2double val_dcm_dhi)
 Value of the weight of the CD, CL, CM optimization. More...
 
void SetdCD_dCMy (su2double val_dcd_dcmy)
 Value of the weight of the CD, CL, CM optimization. More...
 
su2double GetCL_Target (void)
 Value of the weight of the CD, CL, CM optimization. More...
 
void SetGlobalParam (unsigned short val_solver, unsigned short val_system, unsigned long val_extiter)
 Set the global parameters of each simulation for each runtime system. More...
 
su2doubleGetPeriodicRotCenter (string val_marker)
 Center of rotation for a rotational periodic boundary. More...
 
su2doubleGetPeriodicRotAngles (string val_marker)
 Angles of rotation for a rotational periodic boundary. More...
 
su2doubleGetPeriodicTranslation (string val_marker)
 Translation vector for a rotational periodic boundary. More...
 
unsigned short GetMarker_Periodic_Donor (string val_marker)
 Get the rotationally periodic donor marker for boundary val_marker. More...
 
su2double GetActDisk_NetThrust (string val_marker)
 Get the origin of the actuator disk. More...
 
su2double GetActDisk_Power (string val_marker)
 Get the origin of the actuator disk. More...
 
su2double GetActDisk_MassFlow (string val_marker)
 Get the origin of the actuator disk. More...
 
su2double GetActDisk_Mach (string val_marker)
 Get the origin of the actuator disk. More...
 
su2double GetActDisk_Force (string val_marker)
 Get the origin of the actuator disk. More...
 
su2double GetActDisk_BCThrust (string val_marker)
 Get the origin of the actuator disk. More...
 
su2double GetActDisk_BCThrust_Old (string val_marker)
 Get the origin of the actuator disk. More...
 
su2double GetActDisk_Area (string val_marker)
 Get the tip radius of th actuator disk. More...
 
su2double GetActDisk_ReverseMassFlow (string val_marker)
 Get the tip radius of th actuator disk. More...
 
su2double GetActDisk_PressJump (string val_marker, unsigned short val_index)
 Get the thrust corffient of the actuator disk. More...
 
su2double GetActDisk_TempJump (string val_marker, unsigned short val_index)
 Get the thrust corffient of the actuator disk. More...
 
su2double GetActDisk_Omega (string val_marker, unsigned short val_index)
 Get the rev / min of the actuator disk. More...
 
unsigned short GetMarker_CfgFile_ActDiskOutlet (string val_marker)
 Get Actuator Disk Outlet for boundary val_marker (actuator disk inlet). More...
 
unsigned short GetMarker_CfgFile_EngineExhaust (string val_marker)
 Get Actuator Disk Outlet for boundary val_marker (actuator disk inlet). More...
 
unsigned short GetMarker_Moving (string val_marker)
 Get the internal index for a moving boundary val_marker. More...
 
string GetMarker_Moving_TagBound (unsigned short val_marker)
 Get the name of the surface defined in the geometry file. More...
 
string GetMarker_PyCustom_TagBound (unsigned short val_marker)
 Get the name of the surface defined in the geometry file. More...
 
string GetMarker_Analyze_TagBound (unsigned short val_marker)
 Get the name of the surface defined in the geometry file. More...
 
void SetnPeriodicIndex (unsigned short val_index)
 Set the total number of SEND_RECEIVE periodic transformations. More...
 
unsigned short GetnPeriodicIndex (void)
 Get the total number of SEND_RECEIVE periodic transformations. More...
 
void SetPeriodicCenter (unsigned short val_index, su2double *center)
 Set the rotation center for a periodic transformation. More...
 
su2doubleGetPeriodicCenter (unsigned short val_index)
 Get the rotation center for a periodic transformation. More...
 
void SetPeriodicRotation (unsigned short val_index, su2double *rotation)
 Set the rotation angles for a periodic transformation. More...
 
su2doubleGetPeriodicRotation (unsigned short val_index)
 Get the rotation angles for a periodic transformation. More...
 
void SetPeriodicTranslate (unsigned short val_index, su2double *translate)
 Set the translation vector for a periodic transformation. More...
 
su2doubleGetPeriodicTranslate (unsigned short val_index)
 Get the translation vector for a periodic transformation. More...
 
su2double GetExhaust_Temperature_Target (string val_index)
 Get the total temperature at a nacelle boundary. More...
 
su2double GetInlet_Ttotal (string val_index)
 Get the total temperature at an inlet boundary. More...
 
su2double GetInlet_Temperature (string val_index)
 Get the temperature at a supersonic inlet boundary. More...
 
su2double GetInlet_Pressure (string val_index)
 Get the pressure at a supersonic inlet boundary. More...
 
su2doubleGetInlet_Velocity (string val_index)
 Get the velocity vector at a supersonic inlet boundary. More...
 
su2double GetDirichlet_Value (string val_index)
 Get the fixed value at the Dirichlet boundary. More...
 
bool GetDirichlet_Boundary (string val_index)
 Get whether this is a Dirichlet or a Neumann boundary. More...
 
su2double GetInlet_Ptotal (string val_index)
 Get the total pressure at an inlet boundary. More...
 
void SetInlet_Ptotal (su2double val_pressure, string val_marker)
 Set the total pressure at an inlet boundary. More...
 
su2double GetExhaust_Pressure_Target (string val_index)
 Get the total pressure at an nacelle boundary. More...
 
su2double GetCFLRedCoeff_Turb (void)
 Value of the CFL reduction in LevelSet problems. More...
 
su2doubleGetInlet_FlowDir (string val_index)
 Get the flow direction unit vector at an inlet boundary. More...
 
su2double GetOutlet_Pressure (string val_index)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetOutlet_Pressure (su2double val_pressure, string val_marker)
 Set the back pressure (static) at an outlet boundary. More...
 
su2double GetRiemann_Var1 (string val_marker)
 Get the var 1 at Riemann boundary. More...
 
su2double GetRiemann_Var2 (string val_marker)
 Get the var 2 at Riemann boundary. More...
 
su2doubleGetRiemann_FlowDir (string val_marker)
 Get the Flowdir at Riemann boundary. More...
 
unsigned short GetKind_Data_Riemann (string val_marker)
 Get Kind Data of Riemann boundary. More...
 
su2double GetGiles_Var1 (string val_marker)
 Get the var 1 for the Giels BC. More...
 
su2double GetGiles_Var2 (string val_marker)
 Get the var 2 for the Giles boundary. More...
 
su2doubleGetGiles_FlowDir (string val_marker)
 Get the Flowdir for the Giles BC. More...
 
unsigned short GetKind_Data_Giles (string val_marker)
 Get Kind Data for the Giles BC. More...
 
void SetGiles_Var1 (su2double newVar1, string val_marker)
 Set the var 1 for Giles BC. More...
 
su2double GetGiles_RelaxFactorAverage (string val_marker)
 Get the relax factor for the average component for the Giles BC. More...
 
su2double GetGiles_RelaxFactorFourier (string val_marker)
 Get the relax factor for the fourier component for the Giles BC. More...
 
su2double GetPressureOut_BC ()
 Get the outlet pressure imposed as BC for internal flow. More...
 
void SetPressureOut_BC (su2double val_press)
 Set the outlet pressure imposed as BC for internal flow. More...
 
su2double GetIncInlet_BC ()
 Get the inlet velocity or pressure imposed for incompressible flow. More...
 
void SetIncInlet_BC (su2double val_in)
 Set the inlet velocity or pressure imposed as BC for incompressible flow. More...
 
su2double GetIncTemperature_BC ()
 Get the inlet temperature imposed as BC for incompressible flow. More...
 
void SetIncTemperature_BC (su2double val_temperature)
 Set the inlet temperature imposed as BC for incompressible flow. More...
 
su2double GetIncPressureOut_BC ()
 Get the outlet pressure imposed as BC for incompressible flow. More...
 
void SetIncPressureOut_BC (su2double val_pressure)
 Set the outlet pressure imposed as BC for incompressible flow. More...
 
su2double GetTotalPressureIn_BC ()
 Get the inlet total pressure imposed as BC for internal flow. More...
 
su2double GetTotalTemperatureIn_BC ()
 Get the inlet total temperature imposed as BC for internal flow. More...
 
void SetTotalTemperatureIn_BC (su2double val_temp)
 Set the inlet total temperature imposed as BC for internal flow. More...
 
su2double GetFlowAngleIn_BC ()
 Get the inlet flow angle imposed as BC for internal flow. More...
 
su2double GetIsothermal_Temperature (string val_index)
 Get the wall temperature (static) at an isothermal boundary. More...
 
su2double GetWall_HeatFlux (string val_index)
 Get the wall heat flux on a constant heat flux boundary. More...
 
void GetTranspirationParams (string val_marker, su2double &x0, su2double &x1, su2double &x2, su2double &x3, su2double &y0, su2double &y1, su2double &y2, su2double &y3, su2double &eps0, su2double &eps1, su2double &eps2, su2double &eps3)
 Get the wall transpiration parameters. More...
 
void SetTranspirationParams_DV ()
 Set the transpiration params using DV values. More...
 
string GetTranspirationFileName ()
 Get the name of file containing all transpirations. More...
 
unsigned short GetWallFunction_Treatment (string val_marker)
 Get the wall function treatment for the given boundary marker. More...
 
unsigned short * GetWallFunction_IntInfo (string val_marker)
 Get the additional integer info for the wall function treatment for the given boundary marker. More...
 
su2doubleGetWallFunction_DoubleInfo (string val_marker)
 Get the additional double info for the wall function treatment for the given boundary marker. More...
 
su2double GetEngineInflow_Target (string val_marker)
 Get the target (pressure, massflow, etc) at an engine inflow boundary. More...
 
su2double GetInflow_Mach (string val_marker)
 Get the fan face Mach number at an engine inflow boundary. More...
 
su2double GetInflow_Pressure (string val_marker)
 Get the back pressure (static) at an engine inflow boundary. More...
 
su2double GetInflow_MassFlow (string val_marker)
 Get the mass flow rate at an engine inflow boundary. More...
 
su2double GetInflow_ReverseMassFlow (string val_marker)
 Get the percentage of reverse flow at an engine inflow boundary. More...
 
su2double GetInflow_ReverseMassFlow (unsigned short val_marker)
 Get the percentage of reverse flow at an engine inflow boundary. More...
 
su2double GetInflow_TotalPressure (string val_marker)
 Get the total pressure at an engine inflow boundary. More...
 
su2double GetInflow_Temperature (string val_marker)
 Get the temperature (static) at an engine inflow boundary. More...
 
su2double GetInflow_TotalTemperature (string val_marker)
 Get the total temperature at an engine inflow boundary. More...
 
su2double GetInflow_RamDrag (string val_marker)
 Get the ram drag at an engine inflow boundary. More...
 
su2double GetInflow_Force (string val_marker)
 Get the force balance at an engine inflow boundary. More...
 
su2double GetInflow_Power (string val_marker)
 Get the power at an engine inflow boundary. More...
 
su2double GetExhaust_Pressure (string val_marker)
 Get the back pressure (static) at an engine exhaust boundary. More...
 
su2double GetExhaust_Temperature (string val_marker)
 Get the temperature (static) at an engine exhaust boundary. More...
 
su2double GetExhaust_MassFlow (string val_marker)
 Get the massflow at an engine exhaust boundary. More...
 
su2double GetExhaust_TotalPressure (string val_marker)
 Get the total pressure at an engine exhaust boundary. More...
 
su2double GetExhaust_TotalTemperature (string val_marker)
 Get the total temperature at an engine exhaust boundary. More...
 
su2double GetExhaust_GrossThrust (string val_marker)
 Get the gross thrust at an engine exhaust boundary. More...
 
su2double GetExhaust_Force (string val_marker)
 Get the force balance at an engine exhaust boundary. More...
 
su2double GetExhaust_Power (string val_marker)
 Get the power at an engine exhaust boundary. More...
 
void SetInflow_Mach (unsigned short val_imarker, su2double val_fanface_mach)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetInflow_Pressure (unsigned short val_imarker, su2double val_fanface_pressure)
 Set the fan face static pressure at an engine inflow boundary. More...
 
void SetInflow_MassFlow (unsigned short val_imarker, su2double val_fanface_massflow)
 Set the massflow at an engine inflow boundary. More...
 
void SetInflow_ReverseMassFlow (unsigned short val_imarker, su2double val_fanface_reversemassflow)
 Set the reverse flow at an engine inflow boundary. More...
 
void SetInflow_TotalPressure (unsigned short val_imarker, su2double val_fanface_totalpressure)
 Set the fan face total pressure at an engine inflow boundary. More...
 
void SetInflow_Temperature (unsigned short val_imarker, su2double val_fanface_temperature)
 Set the fan face static temperature at an engine inflow boundary. More...
 
void SetInflow_TotalTemperature (unsigned short val_imarker, su2double val_fanface_totaltemperature)
 Set the fan face total temperature at an engine inflow boundary. More...
 
void SetInflow_RamDrag (unsigned short val_imarker, su2double val_fanface_ramdrag)
 Set the ram drag temperature at an engine inflow boundary. More...
 
void SetInflow_Force (unsigned short val_imarker, su2double val_fanface_force)
 Set the force balance at an engine inflow boundary. More...
 
void SetInflow_Power (unsigned short val_imarker, su2double val_fanface_power)
 Set the power at an engine inflow boundary. More...
 
void SetExhaust_Pressure (unsigned short val_imarker, su2double val_exhaust_pressure)
 Set the back pressure (static) at an engine exhaust boundary. More...
 
void SetExhaust_Temperature (unsigned short val_imarker, su2double val_exhaust_temp)
 Set the temperature (static) at an engine exhaust boundary. More...
 
void SetExhaust_MassFlow (unsigned short val_imarker, su2double val_exhaust_massflow)
 Set the back pressure (static) at an engine exhaust boundary. More...
 
void SetExhaust_TotalPressure (unsigned short val_imarker, su2double val_exhaust_totalpressure)
 Set the back pressure (total) at an engine exhaust boundary. More...
 
void SetExhaust_TotalTemperature (unsigned short val_imarker, su2double val_exhaust_totaltemp)
 Set the total temperature at an engine exhaust boundary. More...
 
void SetExhaust_GrossThrust (unsigned short val_imarker, su2double val_exhaust_grossthrust)
 Set the gross thrust at an engine exhaust boundary. More...
 
void SetExhaust_Force (unsigned short val_imarker, su2double val_exhaust_force)
 Set the force balance at an engine exhaust boundary. More...
 
void SetExhaust_Power (unsigned short val_imarker, su2double val_exhaust_power)
 Set the power at an engine exhaust boundary. More...
 
void SetEngine_Mach (unsigned short val_imarker, su2double val_engine_mach)
 Set the back pressure (static) at an outlet boundary. More...
 
void SetEngine_Force (unsigned short val_imarker, su2double val_engine_force)
 Set the back pressure (static) at an outlet boundary. More...
 
void SetEngine_Power (unsigned short val_imarker, su2double val_engine_power)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetEngine_NetThrust (unsigned short val_imarker, su2double val_engine_netthrust)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetEngine_GrossThrust (unsigned short val_imarker, su2double val_engine_grossthrust)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetEngine_Area (unsigned short val_imarker, su2double val_engine_area)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetEngine_Mach (unsigned short val_imarker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetEngine_Force (unsigned short val_imarker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetEngine_Power (unsigned short val_imarker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetEngine_NetThrust (unsigned short val_imarker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetEngine_GrossThrust (unsigned short val_imarker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetEngine_Area (unsigned short val_imarker)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDiskInlet_Temperature (unsigned short val_imarker, su2double val_actdisk_temp)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDiskInlet_TotalTemperature (unsigned short val_imarker, su2double val_actdisk_totaltemp)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDiskInlet_Temperature (string val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDiskInlet_TotalTemperature (string val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDiskOutlet_Temperature (unsigned short val_imarker, su2double val_actdisk_temp)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDiskOutlet_TotalTemperature (unsigned short val_imarker, su2double val_actdisk_totaltemp)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDiskOutlet_Temperature (string val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDiskOutlet_TotalTemperature (string val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDiskInlet_MassFlow (string val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDiskInlet_MassFlow (unsigned short val_imarker, su2double val_actdisk_massflow)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDiskOutlet_MassFlow (string val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDiskOutlet_MassFlow (unsigned short val_imarker, su2double val_actdisk_massflow)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDiskInlet_Pressure (string val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDiskInlet_TotalPressure (string val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDisk_DeltaPress (unsigned short val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDisk_DeltaTemp (unsigned short val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDisk_TotalPressRatio (unsigned short val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDisk_TotalTempRatio (unsigned short val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDisk_StaticPressRatio (unsigned short val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDisk_StaticTempRatio (unsigned short val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDisk_NetThrust (unsigned short val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDisk_BCThrust (unsigned short val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDisk_BCThrust_Old (unsigned short val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDisk_GrossThrust (unsigned short val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDisk_Area (unsigned short val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDisk_ReverseMassFlow (unsigned short val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDiskInlet_RamDrag (string val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDiskInlet_Force (string val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDiskInlet_Power (string val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDiskInlet_Pressure (unsigned short val_imarker, su2double val_actdisk_pressure)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDiskInlet_TotalPressure (unsigned short val_imarker, su2double val_actdisk_totalpressure)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDisk_DeltaPress (unsigned short val_imarker, su2double val_actdisk_deltapress)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDisk_Power (unsigned short val_imarker, su2double val_actdisk_power)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDisk_MassFlow (unsigned short val_imarker, su2double val_actdisk_massflow)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDisk_Mach (unsigned short val_imarker, su2double val_actdisk_mach)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDisk_Force (unsigned short val_imarker, su2double val_actdisk_force)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetSurface_DC60 (unsigned short val_imarker, su2double val_surface_distortion)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetSurface_MassFlow (unsigned short val_imarker, su2double val_surface_massflow)
 Set the massflow at the surface. More...
 
void SetSurface_Mach (unsigned short val_imarker, su2double val_surface_mach)
 Set the mach number at the surface. More...
 
void SetSurface_Temperature (unsigned short val_imarker, su2double val_surface_temperature)
 Set the temperature at the surface. More...
 
void SetSurface_Pressure (unsigned short val_imarker, su2double val_surface_pressure)
 Set the pressure at the surface. More...
 
void SetSurface_Density (unsigned short val_imarker, su2double val_surface_density)
 Set the density at the surface. More...
 
void SetSurface_Enthalpy (unsigned short val_imarker, su2double val_surface_enthalpy)
 Set the enthalpy at the surface. More...
 
void SetSurface_NormalVelocity (unsigned short val_imarker, su2double val_surface_normalvelocity)
 Set the normal velocity at the surface. More...
 
void SetSurface_Uniformity (unsigned short val_imarker, su2double val_surface_streamwiseuniformity)
 Set the streamwise flow uniformity at the surface. More...
 
void SetSurface_SecondaryStrength (unsigned short val_imarker, su2double val_surface_secondarystrength)
 Set the secondary flow strength at the surface. More...
 
void SetSurface_SecondOverUniform (unsigned short val_imarker, su2double val_surface_secondaryoverstream)
 Set the relative secondary flow strength at the surface. More...
 
void SetSurface_MomentumDistortion (unsigned short val_imarker, su2double val_surface_momentumdistortion)
 Set the momentum distortion at the surface. More...
 
void SetSurface_TotalTemperature (unsigned short val_imarker, su2double val_surface_totaltemperature)
 Set the total temperature at the surface. More...
 
void SetSurface_TotalPressure (unsigned short val_imarker, su2double val_surface_totalpressure)
 Set the total pressure at the surface. More...
 
void SetSurface_PressureDrop (unsigned short val_imarker, su2double val_surface_pressuredrop)
 Set the pressure drop between two surfaces. More...
 
void SetSurface_IDC (unsigned short val_imarker, su2double val_surface_distortion)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetSurface_IDC_Mach (unsigned short val_imarker, su2double val_surface_distortion)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetSurface_IDR (unsigned short val_imarker, su2double val_surface_distortion)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDisk_DeltaTemp (unsigned short val_imarker, su2double val_actdisk_deltatemp)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDisk_TotalPressRatio (unsigned short val_imarker, su2double val_actdisk_pressratio)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDisk_TotalTempRatio (unsigned short val_imarker, su2double val_actdisk_tempratio)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDisk_StaticPressRatio (unsigned short val_imarker, su2double val_actdisk_pressratio)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDisk_StaticTempRatio (unsigned short val_imarker, su2double val_actdisk_tempratio)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDisk_NetThrust (unsigned short val_imarker, su2double val_actdisk_netthrust)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDisk_BCThrust (string val_marker, su2double val_actdisk_bcthrust)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDisk_BCThrust (unsigned short val_imarker, su2double val_actdisk_bcthrust)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDisk_BCThrust_Old (string val_marker, su2double val_actdisk_bcthrust_old)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDisk_BCThrust_Old (unsigned short val_imarker, su2double val_actdisk_bcthrust_old)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDisk_GrossThrust (unsigned short val_imarker, su2double val_actdisk_grossthrust)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDisk_Area (unsigned short val_imarker, su2double val_actdisk_area)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDiskInlet_ReverseMassFlow (unsigned short val_imarker, su2double val_actdisk_area)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDiskInlet_RamDrag (unsigned short val_imarker, su2double val_actdisk_ramdrag)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDiskInlet_Force (unsigned short val_imarker, su2double val_actdisk_force)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDiskInlet_Power (unsigned short val_imarker, su2double val_actdisk_power)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDisk_Power (unsigned short val_imarker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDisk_MassFlow (unsigned short val_imarker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDisk_Mach (unsigned short val_imarker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDisk_Force (unsigned short val_imarker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetSurface_DC60 (unsigned short val_imarker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetSurface_MassFlow (unsigned short val_imarker)
 Get the massflow at an outlet boundary. More...
 
su2double GetSurface_Mach (unsigned short val_imarker)
 Get the mach number at an outlet boundary. More...
 
su2double GetSurface_Temperature (unsigned short val_imarker)
 Get the temperature at an outlet boundary. More...
 
su2double GetSurface_Pressure (unsigned short val_imarker)
 Get the pressure at an outlet boundary. More...
 
su2double GetSurface_Density (unsigned short val_imarker)
 Get the density at an outlet boundary. More...
 
su2double GetSurface_Enthalpy (unsigned short val_imarker)
 Get the enthalpy at an outlet boundary. More...
 
su2double GetSurface_NormalVelocity (unsigned short val_imarker)
 Get the normal velocity at an outlet boundary. More...
 
su2double GetSurface_Uniformity (unsigned short val_imarker)
 Get the streamwise flow uniformity at the surface. More...
 
su2double GetSurface_SecondaryStrength (unsigned short val_imarker)
 Get the secondary flow strength at the surface. More...
 
su2double GetSurface_SecondOverUniform (unsigned short val_imarker)
 Get the relative secondary flow strength at the surface. More...
 
su2double GetSurface_MomentumDistortion (unsigned short val_imarker)
 Get the momentum distortion at the surface. More...
 
su2double GetSurface_TotalTemperature (unsigned short val_imarker)
 Get the total temperature at an outlet boundary. More...
 
su2double GetSurface_TotalPressure (unsigned short val_imarker)
 Get the total pressure at an outlet boundary. More...
 
su2double GetSurface_PressureDrop (unsigned short val_imarker)
 Get the pressure drop between two surfaces. More...
 
su2double GetSurface_IDC (unsigned short val_imarker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetSurface_IDC_Mach (unsigned short val_imarker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetSurface_IDR (unsigned short val_imarker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDiskOutlet_Pressure (string val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDiskOutlet_TotalPressure (string val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDiskOutlet_GrossThrust (string val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDiskOutlet_Force (string val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetActDiskOutlet_Power (string val_marker)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDiskOutlet_Pressure (unsigned short val_imarker, su2double val_actdisk_pressure)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDiskOutlet_TotalPressure (unsigned short val_imarker, su2double val_actdisk_totalpressure)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDiskOutlet_GrossThrust (unsigned short val_imarker, su2double val_actdisk_grossthrust)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDiskOutlet_Force (unsigned short val_imarker, su2double val_actdisk_force)
 Get the back pressure (static) at an outlet boundary. More...
 
void SetActDiskOutlet_Power (unsigned short val_imarker, su2double val_actdisk_power)
 Get the back pressure (static) at an outlet boundary. More...
 
su2double GetDispl_Value (string val_index)
 Get the displacement value at an displacement boundary. More...
 
su2double GetLoad_Value (string val_index)
 Get the force value at an load boundary. More...
 
su2double GetDamper_Constant (string val_index)
 Get the constant value at a damper boundary. More...
 
su2double GetLoad_Dir_Value (string val_index)
 Get the force value at a load boundary defined in cartesian coordinates. More...
 
su2double GetLoad_Dir_Multiplier (string val_index)
 Get the force multiplier at a load boundary in cartesian coordinates. More...
 
su2double GetDisp_Dir_Value (string val_index)
 Get the force value at a load boundary defined in cartesian coordinates. More...
 
su2double GetDisp_Dir_Multiplier (string val_index)
 Get the force multiplier at a load boundary in cartesian coordinates. More...
 
su2doubleGetLoad_Dir (string val_index)
 Get the force direction at a loaded boundary in cartesian coordinates. More...
 
su2doubleGetDisp_Dir (string val_index)
 Get the force direction at a loaded boundary in cartesian coordinates. More...
 
su2double GetLoad_Sine_Amplitude (string val_index)
 Get the amplitude of the sine-wave at a load boundary defined in cartesian coordinates. More...
 
su2double GetLoad_Sine_Frequency (string val_index)
 Get the frequency of the sine-wave at a load boundary in cartesian coordinates. More...
 
su2doubleGetLoad_Sine_Dir (string val_index)
 Get the force direction at a sine-wave loaded boundary in cartesian coordinates. More...
 
su2double GetFlowLoad_Value (string val_index)
 Get the force value at an load boundary. More...
 
su2double GetCyclic_Pitch (void)
 Cyclic pitch amplitude for rotor blades. More...
 
su2double GetCollective_Pitch (void)
 Collective pitch setting for rotor blades. More...
 
string GetDV_Filename (void)
 Get name of the arbitrary mesh motion input file. More...
 
void SetConfig_Options (unsigned short val_iZone, unsigned short val_nZone)
 Set the config options. More...
 
void SetRunTime_Options (void)
 Set the config options. More...
 
void SetConfig_Parsing (char case_filename[MAX_STRING_SIZE])
 Set the config file parsing. More...
 
bool SetRunTime_Parsing (char case_filename[MAX_STRING_SIZE])
 Set the config file parsing. More...
 
void SetPostprocessing (unsigned short val_software, unsigned short val_izone, unsigned short val_nDim)
 Config file postprocessing. More...
 
void SetMarkers (unsigned short val_software)
 Config file markers processing. More...
 
void SetOutput (unsigned short val_software, unsigned short val_izone)
 Config file output. More...
 
vector< vector< su2double > > GetAeroelastic_np1 (unsigned short iMarker)
 Value of Aeroelastic solution coordinate at time n+1. More...
 
vector< vector< su2double > > GetAeroelastic_n (unsigned short iMarker)
 Value of Aeroelastic solution coordinate at time n. More...
 
vector< vector< su2double > > GetAeroelastic_n1 (unsigned short iMarker)
 Value of Aeroelastic solution coordinate at time n-1. More...
 
void SetAeroelastic_np1 (unsigned short iMarker, vector< vector< su2double > > solution)
 Value of Aeroelastic solution coordinate at time n+1. More...
 
void SetAeroelastic_n (void)
 Value of Aeroelastic solution coordinate at time n from time n+1. More...
 
void SetAeroelastic_n1 (void)
 Value of Aeroelastic solution coordinate at time n-1 from time n. More...
 
su2double GetAeroelastic_Flutter_Speed_Index (void)
 Aeroelastic Flutter Speed Index. More...
 
su2double GetAeroelastic_Frequency_Plunge (void)
 Uncoupled Aeroelastic Frequency Plunge. More...
 
su2double GetAeroelastic_Frequency_Pitch (void)
 Uncoupled Aeroelastic Frequency Pitch. More...
 
su2double GetAeroelastic_Airfoil_Mass_Ratio (void)
 Aeroelastic Airfoil Mass Ratio. More...
 
su2double GetAeroelastic_CG_Location (void)
 Aeroelastic center of gravity location. More...
 
su2double GetAeroelastic_Radius_Gyration_Squared (void)
 Aeroelastic radius of gyration squared. More...
 
unsigned short GetAeroelasticIter (void)
 Aeroelastic solve every x inner iteration. More...
 
su2double GetAeroelastic_plunge (unsigned short val_marker)
 Value of plunging coordinate. More...
 
su2double GetAeroelastic_pitch (unsigned short val_marker)
 Value of pitching coordinate. More...
 
void SetAeroelastic_plunge (unsigned short val_marker, su2double val)
 Value of plunging coordinate. More...
 
void SetAeroelastic_pitch (unsigned short val_marker, su2double val)
 Value of pitching coordinate. More...
 
bool GetAeroelastic_Simulation (void)
 Get information about the aeroelastic simulation. More...
 
bool GetWind_Gust (void)
 Get information about the wind gust. More...
 
unsigned short GetGust_Type (void)
 Get the type of gust to simulate. More...
 
unsigned short GetGust_Dir (void)
 Get the gust direction. More...
 
su2double GetGust_WaveLength (void)
 Value of the gust wavelength. More...
 
su2double GetGust_Periods (void)
 Value of the number of gust periods. More...
 
su2double GetGust_Ampl (void)
 Value of the gust amplitude. More...
 
su2double GetGust_Begin_Time (void)
 Value of the time at which to begin the gust. More...
 
su2double GetGust_Begin_Loc (void)
 Value of the location ath which the gust begins. More...
 
unsigned short GetnFFD_Iter (void)
 Get the number of iterations to evaluate the parametric coordinates. More...
 
su2double GetFFD_Tol (void)
 Get the tolerance of the point inversion algorithm. More...
 
su2double GetOpt_RelaxFactor (void)
 Get the scale factor for the line search. More...
 
su2double GetOpt_LineSearch_Bound (void)
 Get the bound for the line search. More...
 
void SetOpt_RelaxFactor (su2double val_scale)
 Set the scale factor for the line search. More...
 
long GetVisualize_CV (void)
 Get the node number of the CV to visualize. More...
 
bool GetFixed_CL_Mode (void)
 Get information about whether to use fixed CL mode. More...
 
bool GetFixed_CM_Mode (void)
 Get information about whether to use fixed CL mode. More...
 
bool GetEval_dOF_dCX (void)
 Get information about whether to use fixed CL mode. More...
 
bool GetDiscard_InFiles (void)
 Get information about whether to use fixed CL mode. More...
 
su2double GetTarget_CL (void)
 Get the value specified for the target CL. More...
 
su2double GetdCL_dAlpha (void)
 Get the value for the lift curve slope for fixed CL mode. More...
 
unsigned long GetUpdate_Alpha (void)
 Get the value of iterations to re-evaluate the angle of attack. More...
 
unsigned long GetIter_dCL_dAlpha (void)
 Number of iterations to evaluate dCL_dAlpha. More...
 
su2double GetdCM_diH (void)
 Get the value of the damping coefficient for fixed CL mode. More...
 
unsigned long GetIter_Fixed_CL (void)
 Get the value of iterations to re-evaluate the angle of attack. More...
 
unsigned long GetIter_Fixed_NetThrust (void)
 Get the value of iterations to re-evaluate the angle of attack. More...
 
su2double GetdNetThrust_dBCThrust (void)
 Get the value of the damping coefficient for fixed CL mode. More...
 
unsigned long GetUpdate_BCThrust (void)
 Get the value of iterations to re-evaluate the angle of attack. More...
 
void SetUpdate_BCThrust_Bool (bool val_update)
 Set the value of the boolean for updating AoA in fixed lift mode. More...
 
void SetUpdate_AoA (bool val_update)
 Set the value of the boolean for updating AoA in fixed lift mode. More...
 
bool GetUpdate_BCThrust_Bool (void)
 Get information about whether to update the AoA for fixed lift mode. More...
 
bool GetUpdate_AoA (void)
 Get information about whether to update the AoA for fixed lift mode. More...
 
void SetNonphysical_Points (unsigned long val_nonphys_points)
 Set the current number of non-physical nodes in the solution. More...
 
unsigned long GetNonphysical_Points (void)
 Get the current number of non-physical nodes in the solution. More...
 
void SetNonphysical_Reconstr (unsigned long val_nonphys_reconstr)
 Set the current number of non-physical reconstructions for 2nd-order upwinding. More...
 
unsigned long GetNonphysical_Reconstr (void)
 Get the current number of non-physical reconstructions for 2nd-order upwinding. More...
 
void SetSpline (vector< su2double > &x, vector< su2double > &y, unsigned long n, su2double yp1, su2double ypn, vector< su2double > &y2)
 Given arrays x[1..n] and y[1..n] containing a tabulated function, i.e., yi = f(xi), with x1 < x2 < . . . < xN , and given values yp1 and ypn for the first derivative of the interpolating function at points 1 and n, respectively, this routine returns an array y2[1..n] that contains the second derivatives of the interpolating function at the tabulated points xi. If yp1 and/or ypn are equal to 1 × 1030 or larger, the routine is signaled to set the corresponding boundary condition for a natural spline, with zero second derivative on that boundary. Numerical Recipes: The Art of Scientific Computing, Third Edition in C++. More...
 
su2double GetSpline (vector< su2double > &xa, vector< su2double > &ya, vector< su2double > &y2a, unsigned long n, su2double x)
 Given the arrays xa[1..n] and ya[1..n], which tabulate a function (with the xai’s in order), and given the array y2a[1..n], which is the output from spline above, and given a value of x, this routine returns a cubic-spline interpolated value y. Numerical Recipes: The Art of Scientific Computing, Third Edition in C++. More...
 
void Tick (double *val_start_time)
 Start the timer for profiling subroutines. More...
 
void Tock (double val_start_time, string val_function_name, int val_group_id)
 Stop the timer for profiling subroutines and store results. More...
 
void SetProfilingCSV (void)
 Write a CSV file containing the results of the profiling. More...
 
void GEMM_Tick (double *val_start_time)
 Start the timer for profiling subroutines. More...
 
void GEMM_Tock (double val_start_time, int M, int N, int K)
 Stop the timer for the GEMM profiling and store results. More...
 
void GEMMProfilingCSV (void)
 Write a CSV file containing the results of the profiling. More...
 
void SetFreeStreamTurboNormal (su2double *turboNormal)
 Set freestream turbonormal for initializing solution. More...
 
su2doubleGetFreeStreamTurboNormal (void)
 Set freestream turbonormal for initializing solution. More...
 
unsigned short GetConsole_Output_Verb (void)
 Get the verbosity level of the console output. More...
 
unsigned short GetKind_Average (void)
 Get the kind of marker analyze marker (area-averaged, mass flux averaged, etc). More...
 
unsigned short GetDirectDiff ()
 Get the direct differentation method. More...
 
bool GetDiscrete_Adjoint (void)
 Get the indicator whether we are solving an discrete adjoint problem. More...
 
bool CheckFSI_MPI (void)
 Get the indicator whether we want to benchmark the MPI performance of FSI problems. More...
 
unsigned short GetnIterFSI (void)
 Get the number of fluid subiterations roblems. More...
 
unsigned short GetnIterFSI_Ramp (void)
 Get the number of subiterations while a ramp is applied. More...
 
su2double GetAitkenStatRelax (void)
 Get Aitken's relaxation parameter for static relaxation cases. More...
 
su2double GetAitkenDynMaxInit (void)
 Get Aitken's maximum relaxation parameter for dynamic relaxation cases and first iteration. More...
 
su2double GetAitkenDynMinInit (void)
 Get Aitken's maximum relaxation parameter for dynamic relaxation cases and first iteration. More...
 
bool GetDeadLoad (void)
 Decide whether to apply dead loads to the model. More...
 
bool GetPseudoStatic (void)
 Identifies if the mesh is matching or not (temporary, while implementing interpolation procedures). More...
 
bool GetMatchingMesh (void)
 Identifies if the mesh is matching or not (temporary, while implementing interpolation procedures). More...
 
bool GetSteadyRestart (void)
 Identifies if we want to restart from a steady or an unsteady solution. More...
 
unsigned short GetDynamic_Analysis (void)
 Provides information about the time integration of the structural analysis, and change the write in the output files information about the iteration. More...
 
su2double GetDelta_DynTime (void)
 If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation. More...
 
su2double GetTotal_DynTime (void)
 If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation. More...
 
su2double GetCurrent_DynTime (void)
 If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation. More...
 
unsigned short GetiInst (void)
 Get the current instance. More...
 
void SetiInst (unsigned short val_iInst)
 Set the current instance. More...
 
bool GetWrt_Dynamic (void)
 Get information about writing dynamic structural analysis headers and file extensions. More...
 
su2double GetNewmark_beta (void)
 Get Newmark alpha parameter. More...
 
su2double GetNewmark_gamma (void)
 Get Newmark delta parameter. More...
 
unsigned short GetnIntCoeffs (void)
 Get the number of integration coefficients provided by the user. More...
 
unsigned short GetnElasticityMod (void)
 Get the number of different values for the elasticity modulus. More...
 
unsigned short GetnPoissonRatio (void)
 Get the number of different values for the Poisson ratio. More...
 
unsigned short GetnMaterialDensity (void)
 Get the number of different values for the Material density. More...
 
su2double Get_Int_Coeffs (unsigned short val_coeff)
 Get the integration coefficients for the Generalized Alpha - Newmark integration integration scheme. More...
 
unsigned short GetnElectric_Field (void)
 Get the number of different values for the modulus of the electric field. More...
 
unsigned short GetnDim_Electric_Field (void)
 Get the dimensionality of the electric field. More...
 
su2double Get_Electric_Field_Mod (unsigned short val_coeff)
 Get the values for the electric field modulus. More...
 
void Set_Electric_Field_Mod (unsigned short val_coeff, su2double val_el_field)
 Set the values for the electric field modulus. More...
 
su2doubleGet_Electric_Field_Dir (void)
 Get the direction of the electric field in reference configuration. More...
 
bool GetRamp_Load (void)
 Check if the user wants to apply the load as a ramp. More...
 
su2double GetRamp_Time (void)
 Get the maximum time of the ramp. More...
 
bool GetRampAndRelease_Load (void)
 Check if the user wants to apply the load as a ramp. More...
 
bool GetSine_Load (void)
 Check if the user wants to apply the load as a ramp. More...
 
su2doubleGetLoad_Sine (void)
 Get the sine load properties. More...
 
unsigned short GetDynamic_LoadTransfer (void)
 Get the kind of load transfer method we want to use for dynamic problems. More...
 
su2double GetRefGeom_Penalty (void)
 Get the penalty weight value for the objective function. More...
 
su2double GetTotalDV_Penalty (void)
 Get the penalty weight value for the objective function. More...
 
unsigned short GetPredictorOrder (void)
 Get the order of the predictor for FSI applications. More...
 
bool GetEulerPersson (void)
 Get boolean for using Persson's shock capturing method in Euler flow DG-FEM. More...
 
void SetEulerPersson (bool val_EulerPersson)
 Set boolean for using Persson's shock capturing method in Euler flow DG-FEM. More...
 
bool GetFSI_Simulation (void)
 Check if the simulation we are running is a FSI simulation. More...
 
unsigned short GetnID_DV (void)
 Get the ID for the FEA region that we want to compute the gradient for using direct differentiation. More...
 
bool GetIncrementalLoad (void)
 Check if we want to apply an incremental load to the nonlinear structural simulation. More...
 
unsigned long GetNumberIncrements (void)
 Get the number of increments for an incremental load. More...
 
su2double GetIncLoad_Criteria (unsigned short val_var)
 Get the value of the criteria for applying incremental loading. More...
 
unsigned short GetRelaxation_Method_FSI (void)
 Get the relaxation method chosen for the simulation. More...
 
unsigned short GetRiemann_Solver_FEM (void)
 Get the kind of Riemann solver for the DG method (FEM flow solver). More...
 
su2double GetQuadrature_Factor_Straight (void)
 Get the factor applied during quadrature of straight elements. More...
 
su2double GetQuadrature_Factor_Curved (void)
 Get the factor applied during quadrature of curved elements. More...
 
su2double GetQuadrature_Factor_Time_ADER_DG (void)
 Get the factor applied during time quadrature for ADER-DG. More...
 
su2double GetTheta_Interior_Penalty_DGFEM (void)
 Function to make available the multiplication factor theta of the symmetrizing terms in the DG discretization of the viscous terms. More...
 
unsigned short GetSizeMatMulPadding (void)
 Function to make available the matrix size in vectorization in order to optimize the gemm performance. More...
 
bool GetCompute_Entropy (void)
 Function to make available whether or not the entropy must be computed. More...
 
bool GetUse_Lumped_MassMatrix_DGFEM (void)
 Function to make available whether or not the lumped mass matrix must be used for steady computations. More...
 
bool GetJacobian_Spatial_Discretization_Only (void)
 Function to make available whether or not only the exact Jacobian of the spatial discretization must be computed. More...
 
unsigned short GetKindInterpolation (void)
 Get the interpolation method used for matching between zones. More...
 
bool GetConservativeInterpolation (void)
 Get option of whether to use conservative interpolation between zones. More...
 
unsigned short GetKindRadialBasisFunction (void)
 Get the basis function to use for radial basis function interpolation for FSI. More...
 
bool GetRadialBasisFunctionPolynomialOption (void)
 Get option of whether to use polynomial terms in Radial Basis Function interpolation. More...
 
su2double GetRadialBasisFunctionParameter (void)
 Get the basis function radius to use for radial basis function interpolation for FSI. More...
 
bool GetWall_Functions (void)
 Get information about whether to use wall functions. More...
 
bool GetAD_Mode (void)
 Get the AD support. More...
 
void SetMax_Vel2 (su2double val_max_vel2)
 Set the maximum velocity^2 in the domain for the incompressible preconditioner. More...
 
su2double GetMax_Vel2 (void)
 Get the maximum velocity^2 in the domain for the incompressible preconditioner. More...
 
void SetRestart_Bandwidth_Agg (su2double val_restart_bandwidth_sum)
 Set the sum of the bandwidth for writing binary restarts (to be averaged later). More...
 
su2double GetRestart_Bandwidth_Agg (void)
 Set the sum of the bandwidth for writing binary restarts (to be averaged later). More...
 
unsigned long GetWrt_Surf_Freq_DualTime (void)
 Get the frequency for writing the surface solution file in Dual Time. More...
 
unsigned short GetKind_HybridRANSLES (void)
 Get the Kind of Hybrid RANS/LES. More...
 
unsigned short GetKind_RoeLowDiss (void)
 Get the Kind of Roe Low Dissipation Scheme for Unsteady flows. More...
 
su2double GetConst_DES (void)
 Get the DES Constant. More...
 
bool GetQCR (void)
 Get QCR (SA-QCR2000). More...
 
bool GetAD_Preaccumulation (void)
 Get if AD preaccumulation should be performed. More...
 
bool GetWeakly_Coupled_Heat (void)
 Get the heat equation. More...
 
bool GetIntegrated_HeatFlux (void)
 Check if values passed to the BC_HeatFlux-Routine are already integrated. More...
 
ofstream * GetHistFile (void)
 Retrieve the ofstream of the history file for the current zone. More...
 
void SetHistFile (ofstream *HistFile)
 Set the ofstream of the history file for the current zone. More...
 
bool GetCompute_Average (void)
 Get Compute Average. More...
 

Static Public Member Functions

static unsigned short GetnZone (string val_mesh_filename, unsigned short val_format, CConfig *config)
 Gets the number of zones in the mesh file. More...
 
static unsigned short GetnDim (string val_mesh_filename, unsigned short val_format)
 Gets the number of dimensions in the mesh file. More...
 
static bool GetPeriodic (string val_mesh_filename, unsigned short val_format, CConfig *config)
 Determine whether there are periodic BCs in the grid. More...
 

Public Attributes

vector< string > fields
 Tags for the different fields in a restart file. More...
 

Detailed Description

Main class for defining the problem; basically this class reads the configuration file, and stores all the information.

Author
F. Palacios

Definition at line 71 of file config_structure.hpp.

Constructor & Destructor Documentation

◆ CConfig() [1/3]

CConfig::CConfig ( char  case_filename[MAX_STRING_SIZE],
unsigned short  val_software,
unsigned short  val_iZone,
unsigned short  val_nZone,
unsigned short  val_nDim,
unsigned short  verb_level 
)

Constructor of the class which reads the input file.

Definition at line 60 of file config_structure.cpp.

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◆ CConfig() [2/3]

CConfig::CConfig ( char  case_filename[MAX_STRING_SIZE],
unsigned short  val_software 
)

Constructor of the class which reads the input file.

Definition at line 94 of file config_structure.cpp.

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◆ CConfig() [3/3]

CConfig::CConfig ( char  case_filename[MAX_STRING_SIZE],
CConfig config 
)

Constructor of the class which reads the input file.

Definition at line 123 of file config_structure.cpp.

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◆ ~CConfig()

CConfig::~CConfig ( void  )

Destructor of the class.

Definition at line 6585 of file config_structure.cpp.

Member Function Documentation

◆ Add_CrossTerm()

bool CConfig::Add_CrossTerm ( void  )
inline

Decide whether it's necessary to add the cross term for adjoint FSI.

Returns
TRUE if it's necessary to add the cross term, FALSE otherwise.

Definition at line 410 of file config_structure.inl.

◆ CheckFSI_MPI()

bool CConfig::CheckFSI_MPI ( void  )

Get the indicator whether we want to benchmark the MPI performance of FSI problems.

Returns
The value for checking

◆ GEMM_Tick()

void CConfig::GEMM_Tick ( double *  val_start_time)

Start the timer for profiling subroutines.

Parameters
[in]val_start_time- the value of the start time.

Definition at line 8676 of file config_structure.cpp.

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◆ GEMM_Tock()

void CConfig::GEMM_Tock ( double  val_start_time,
int  M,
int  N,
int  K 
)

Stop the timer for the GEMM profiling and store results.

Parameters
[in]val_start_time- The value of the start time.
[in]M,N,K- Matrix size of the GEMM call.

Definition at line 8692 of file config_structure.cpp.

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◆ GEMMProfilingCSV()

void CConfig::GEMMProfilingCSV ( void  )

Write a CSV file containing the results of the profiling.

Definition at line 8741 of file config_structure.cpp.

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◆ Get_Alpha_RKStep()

su2double CConfig::Get_Alpha_RKStep ( unsigned short  val_step)
inline

Get the alpha (convective) coefficients for the Runge-Kutta integration scheme.

Parameters
[in]val_step- Index of the step.
Returns
Alpha coefficient for the Runge-Kutta integration scheme.

Definition at line 801 of file config_structure.inl.

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◆ Get_Electric_Field_Dir()

su2double * CConfig::Get_Electric_Field_Dir ( void  )
inline

Get the direction of the electric field in reference configuration.

Parameters
[in]val_coeff- Index of the coefficient.
Returns
Alpha coefficient for the Runge-Kutta integration scheme.

Definition at line 1843 of file config_structure.inl.

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◆ Get_Electric_Field_Mod()

su2double CConfig::Get_Electric_Field_Mod ( unsigned short  val_coeff)
inline

Get the values for the electric field modulus.

Parameters
[in]val_coeff- Index of the coefficient.
Returns
Alpha coefficient for the Runge-Kutta integration scheme.

Definition at line 1839 of file config_structure.inl.

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◆ Get_Int_Coeffs()

su2double CConfig::Get_Int_Coeffs ( unsigned short  val_coeff)
inline

Get the integration coefficients for the Generalized Alpha - Newmark integration integration scheme.

Parameters
[in]val_coeff- Index of the coefficient.
Returns
Alpha coefficient for the Runge-Kutta integration scheme.

Definition at line 1833 of file config_structure.inl.

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◆ Get_nSpanWiseSections_User()

unsigned short CConfig::Get_nSpanWiseSections_User ( void  )
inline

number span-wise sections to compute 3D BC and performance for turbomachinery specified by the user.

Returns
number of span-wise sections.

Definition at line 1244 of file config_structure.inl.

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◆ GetAcentric_Factor()

su2double CConfig::GetAcentric_Factor ( void  )
inline

Get the value of the critical pressure.

Returns
Critical pressure.

Definition at line 870 of file config_structure.inl.

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◆ GetActDisk_Area() [1/2]

su2double CConfig::GetActDisk_Area ( string  val_marker)

Get the tip radius of th actuator disk.

Definition at line 7503 of file config_structure.cpp.

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◆ GetActDisk_Area() [2/2]

su2double CConfig::GetActDisk_Area ( unsigned short  val_marker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 230 of file config_structure.inl.

◆ GetActDisk_BCThrust() [1/2]

su2double CConfig::GetActDisk_BCThrust ( string  val_marker)

Get the origin of the actuator disk.

Definition at line 7471 of file config_structure.cpp.

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◆ GetActDisk_BCThrust() [2/2]

su2double CConfig::GetActDisk_BCThrust ( unsigned short  val_marker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 224 of file config_structure.inl.

◆ GetActDisk_BCThrust_Old() [1/2]

su2double CConfig::GetActDisk_BCThrust_Old ( string  val_marker)

Get the origin of the actuator disk.

Definition at line 7479 of file config_structure.cpp.

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◆ GetActDisk_BCThrust_Old() [2/2]

su2double CConfig::GetActDisk_BCThrust_Old ( unsigned short  val_marker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 226 of file config_structure.inl.

◆ GetActDisk_DeltaPress()

su2double CConfig::GetActDisk_DeltaPress ( unsigned short  val_marker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 166 of file config_structure.inl.

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◆ GetActDisk_DeltaTemp()

su2double CConfig::GetActDisk_DeltaTemp ( unsigned short  val_marker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 168 of file config_structure.inl.

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◆ GetActDisk_DoubleSurface()

bool CConfig::GetActDisk_DoubleSurface ( void  )
inline

Actuator disk defined with a double surface.

Returns
TRUE if the elements must be divided; otherwise FALSE.

Definition at line 1519 of file config_structure.inl.

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◆ GetActDisk_Force() [1/2]

su2double CConfig::GetActDisk_Force ( string  val_marker)

Get the origin of the actuator disk.

Definition at line 7463 of file config_structure.cpp.

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◆ GetActDisk_Force() [2/2]

su2double CConfig::GetActDisk_Force ( unsigned short  val_imarker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 184 of file config_structure.inl.

◆ GetActDisk_GrossThrust()

su2double CConfig::GetActDisk_GrossThrust ( unsigned short  val_marker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 228 of file config_structure.inl.

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◆ GetActDisk_Jump()

unsigned short CConfig::GetActDisk_Jump ( void  )
inline

Get the format of the output solution.

Returns
Format of the output solution.

Definition at line 1437 of file config_structure.inl.

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◆ GetActDisk_Mach() [1/2]

su2double CConfig::GetActDisk_Mach ( string  val_marker)

Get the origin of the actuator disk.

Definition at line 7455 of file config_structure.cpp.

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◆ GetActDisk_Mach() [2/2]

su2double CConfig::GetActDisk_Mach ( unsigned short  val_imarker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 182 of file config_structure.inl.

◆ GetActDisk_MassFlow() [1/2]

su2double CConfig::GetActDisk_MassFlow ( string  val_marker)

Get the origin of the actuator disk.

Definition at line 7447 of file config_structure.cpp.

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◆ GetActDisk_MassFlow() [2/2]

su2double CConfig::GetActDisk_MassFlow ( unsigned short  val_imarker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 180 of file config_structure.inl.

◆ GetActDisk_NetThrust() [1/2]

su2double CConfig::GetActDisk_NetThrust ( string  val_marker)

Get the origin of the actuator disk.

Definition at line 7431 of file config_structure.cpp.

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◆ GetActDisk_NetThrust() [2/2]

su2double CConfig::GetActDisk_NetThrust ( unsigned short  val_marker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 222 of file config_structure.inl.

◆ GetActDisk_Omega()

su2double CConfig::GetActDisk_Omega ( string  val_marker,
unsigned short  val_index 
)

Get the rev / min of the actuator disk.

Definition at line 7535 of file config_structure.cpp.

◆ GetActDisk_Power() [1/2]

su2double CConfig::GetActDisk_Power ( string  val_marker)

Get the origin of the actuator disk.

Definition at line 7439 of file config_structure.cpp.

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◆ GetActDisk_Power() [2/2]

su2double CConfig::GetActDisk_Power ( unsigned short  val_imarker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 178 of file config_structure.inl.

◆ GetActDisk_PressJump()

su2double CConfig::GetActDisk_PressJump ( string  val_marker,
unsigned short  val_index 
)

Get the thrust corffient of the actuator disk.

Definition at line 7519 of file config_structure.cpp.

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◆ GetActDisk_ReverseMassFlow() [1/2]

su2double CConfig::GetActDisk_ReverseMassFlow ( string  val_marker)

Get the tip radius of th actuator disk.

Definition at line 7511 of file config_structure.cpp.

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◆ GetActDisk_ReverseMassFlow() [2/2]

su2double CConfig::GetActDisk_ReverseMassFlow ( unsigned short  val_marker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 232 of file config_structure.inl.

◆ GetActDisk_StaticPressRatio()

su2double CConfig::GetActDisk_StaticPressRatio ( unsigned short  val_marker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 174 of file config_structure.inl.

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◆ GetActDisk_StaticTempRatio()

su2double CConfig::GetActDisk_StaticTempRatio ( unsigned short  val_marker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 176 of file config_structure.inl.

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◆ GetActDisk_SU2_DEF()

bool CConfig::GetActDisk_SU2_DEF ( void  )
inline

Actuator disk defined with a double surface.

Returns
TRUE if the elements must be divided; otherwise FALSE.

Definition at line 1523 of file config_structure.inl.

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◆ GetActDisk_TempJump()

su2double CConfig::GetActDisk_TempJump ( string  val_marker,
unsigned short  val_index 
)

Get the thrust corffient of the actuator disk.

Definition at line 7527 of file config_structure.cpp.

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◆ GetActDisk_TotalPressRatio()

su2double CConfig::GetActDisk_TotalPressRatio ( unsigned short  val_marker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 170 of file config_structure.inl.

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◆ GetActDisk_TotalTempRatio()

su2double CConfig::GetActDisk_TotalTempRatio ( unsigned short  val_marker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 172 of file config_structure.inl.

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◆ GetActDiskInlet_Force()

su2double CConfig::GetActDiskInlet_Force ( string  val_marker)

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 8240 of file config_structure.cpp.

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◆ GetActDiskInlet_MassFlow()

su2double CConfig::GetActDiskInlet_MassFlow ( string  val_marker)

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 8317 of file config_structure.cpp.

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◆ GetActDiskInlet_Power()

su2double CConfig::GetActDiskInlet_Power ( string  val_marker)

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 8247 of file config_structure.cpp.

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◆ GetActDiskInlet_Pressure()

su2double CConfig::GetActDiskInlet_Pressure ( string  val_marker)

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 8219 of file config_structure.cpp.

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◆ GetActDiskInlet_RamDrag()

su2double CConfig::GetActDiskInlet_RamDrag ( string  val_marker)

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 8233 of file config_structure.cpp.

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◆ GetActDiskInlet_Temperature()

su2double CConfig::GetActDiskInlet_Temperature ( string  val_marker)

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 8289 of file config_structure.cpp.

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◆ GetActDiskInlet_TotalPressure()

su2double CConfig::GetActDiskInlet_TotalPressure ( string  val_marker)

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 8226 of file config_structure.cpp.

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◆ GetActDiskInlet_TotalTemperature()

su2double CConfig::GetActDiskInlet_TotalTemperature ( string  val_marker)

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 8296 of file config_structure.cpp.

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◆ GetActDiskOutlet_Force()

su2double CConfig::GetActDiskOutlet_Force ( string  val_marker)

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 8275 of file config_structure.cpp.

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◆ GetActDiskOutlet_GrossThrust()

su2double CConfig::GetActDiskOutlet_GrossThrust ( string  val_marker)

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 8268 of file config_structure.cpp.

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◆ GetActDiskOutlet_MassFlow()

su2double CConfig::GetActDiskOutlet_MassFlow ( string  val_marker)

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 8324 of file config_structure.cpp.

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◆ GetActDiskOutlet_Power()

su2double CConfig::GetActDiskOutlet_Power ( string  val_marker)

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 8282 of file config_structure.cpp.

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◆ GetActDiskOutlet_Pressure()

su2double CConfig::GetActDiskOutlet_Pressure ( string  val_marker)

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 8254 of file config_structure.cpp.

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◆ GetActDiskOutlet_Temperature()

su2double CConfig::GetActDiskOutlet_Temperature ( string  val_marker)

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 8303 of file config_structure.cpp.

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◆ GetActDiskOutlet_TotalPressure()

su2double CConfig::GetActDiskOutlet_TotalPressure ( string  val_marker)

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 8261 of file config_structure.cpp.

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◆ GetActDiskOutlet_TotalTemperature()

su2double CConfig::GetActDiskOutlet_TotalTemperature ( string  val_marker)

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 8310 of file config_structure.cpp.

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◆ GetAD_Mode()

bool CConfig::GetAD_Mode ( void  )
inline

Get the AD support.

Definition at line 1935 of file config_structure.inl.

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◆ GetAD_Preaccumulation()

bool CConfig::GetAD_Preaccumulation ( void  )
inline

Get if AD preaccumulation should be performed.

Definition at line 1937 of file config_structure.inl.

◆ GetAdaptBoundary()

bool CConfig::GetAdaptBoundary ( void  )
inline

Get information about there is a smoothing of the grid coordinates.

Returns
TRUE if there is smoothing of the grid coordinates; otherwise FALSE.

Definition at line 1583 of file config_structure.inl.

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◆ GetAdiabaticWall()

bool CConfig::GetAdiabaticWall ( void  )

Get information about the adibatic wall condition.

Returns
TRUE if it is a adiabatic wall condition; otherwise FALSE.

◆ GetAdj_FileName()

string CConfig::GetAdj_FileName ( void  )
inline

Get the name of the file with the adjoint variables.

Returns
Name of the file with the adjoint variables.

Definition at line 1477 of file config_structure.inl.

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◆ GetAdjointLimit()

su2double CConfig::GetAdjointLimit ( void  )
inline

Get the limit value for the adjoint variables.

Returns
Limit value for the adjoint variables.

Definition at line 336 of file config_structure.inl.

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◆ GetAdjSharp_LimiterCoeff()

su2double CConfig::GetAdjSharp_LimiterCoeff ( void  )
inline

Get the value of sharp edge limiter.

Returns
Value of the sharp edge limiter coefficient.

Definition at line 609 of file config_structure.inl.

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◆ GetAdjStructure_FileName()

string CConfig::GetAdjStructure_FileName ( void  )
inline

Get the name of the file with the adjoint structure variables.

Returns
Name of the file with the adjoint structure variables.

Definition at line 1459 of file config_structure.inl.

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◆ GetAdjSurfStructure_FileName()

string CConfig::GetAdjSurfStructure_FileName ( void  )
inline

Get the name of the file with the adjoint structure variables.

Returns
Name of the file with the adjoint structure variables.

Definition at line 1461 of file config_structure.inl.

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◆ GetAdjTurb_Linear_Error()

su2double CConfig::GetAdjTurb_Linear_Error ( void  )
inline

Get min error of the linear solver for the implicit formulation.

Returns
Min error of the linear solver for the implicit formulation.

Definition at line 1026 of file config_structure.inl.

◆ GetAdjTurb_Linear_Iter()

unsigned short CConfig::GetAdjTurb_Linear_Iter ( void  )
inline

Get max number of iterations of the linear solver for the implicit formulation.

Returns
Max number of iterations of the linear solver for the implicit formulation.

Definition at line 1030 of file config_structure.inl.

◆ GetAeroelastic_Airfoil_Mass_Ratio()

su2double CConfig::GetAeroelastic_Airfoil_Mass_Ratio ( void  )
inline

Aeroelastic Airfoil Mass Ratio.

Definition at line 1709 of file config_structure.inl.

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◆ GetAeroelastic_CG_Location()

su2double CConfig::GetAeroelastic_CG_Location ( void  )
inline

Aeroelastic center of gravity location.

Definition at line 1711 of file config_structure.inl.

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◆ GetAeroelastic_Flutter_Speed_Index()

su2double CConfig::GetAeroelastic_Flutter_Speed_Index ( void  )
inline

Aeroelastic Flutter Speed Index.

Definition at line 1703 of file config_structure.inl.

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◆ GetAeroelastic_Frequency_Pitch()

su2double CConfig::GetAeroelastic_Frequency_Pitch ( void  )
inline

Uncoupled Aeroelastic Frequency Pitch.

Definition at line 1707 of file config_structure.inl.

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◆ GetAeroelastic_Frequency_Plunge()

su2double CConfig::GetAeroelastic_Frequency_Plunge ( void  )
inline

Uncoupled Aeroelastic Frequency Plunge.

Definition at line 1705 of file config_structure.inl.

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◆ GetAeroelastic_n()

vector< vector< su2double > > CConfig::GetAeroelastic_n ( unsigned short  iMarker)
inline

Value of Aeroelastic solution coordinate at time n.

Definition at line 1681 of file config_structure.inl.

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◆ GetAeroelastic_n1()

vector< vector< su2double > > CConfig::GetAeroelastic_n1 ( unsigned short  iMarker)
inline

Value of Aeroelastic solution coordinate at time n-1.

Definition at line 1683 of file config_structure.inl.

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◆ GetAeroelastic_np1()

vector< vector< su2double > > CConfig::GetAeroelastic_np1 ( unsigned short  iMarker)
inline

Value of Aeroelastic solution coordinate at time n+1.

Definition at line 1679 of file config_structure.inl.

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◆ GetAeroelastic_pitch()

su2double CConfig::GetAeroelastic_pitch ( unsigned short  val_marker)
inline

Value of pitching coordinate.

Parameters
[in]val_marker- the marker we are monitoring.
Returns
Value of pitching coordinate.

Definition at line 1689 of file config_structure.inl.

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◆ GetAeroelastic_plunge()

su2double CConfig::GetAeroelastic_plunge ( unsigned short  val_marker)
inline

Value of plunging coordinate.

Parameters
[in]val_marker- the marker we are monitoring.
Returns
Value of plunging coordinate.

Definition at line 1687 of file config_structure.inl.

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◆ GetAeroelastic_Radius_Gyration_Squared()

su2double CConfig::GetAeroelastic_Radius_Gyration_Squared ( void  )
inline

Aeroelastic radius of gyration squared.

Definition at line 1713 of file config_structure.inl.

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◆ GetAeroelastic_Simulation()

bool CConfig::GetAeroelastic_Simulation ( void  )
inline

Get information about the aeroelastic simulation.

Returns
TRUE if it is an aeroelastic case; otherwise FALSE.

Definition at line 1719 of file config_structure.inl.

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◆ GetAeroelasticIter()

unsigned short CConfig::GetAeroelasticIter ( void  )
inline

Aeroelastic solve every x inner iteration.

Definition at line 1715 of file config_structure.inl.

◆ GetAitkenDynMaxInit()

su2double CConfig::GetAitkenDynMaxInit ( void  )
inline

Get Aitken's maximum relaxation parameter for dynamic relaxation cases and first iteration.

Returns
Aitken's relaxation parameters.

Definition at line 1801 of file config_structure.inl.

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◆ GetAitkenDynMinInit()

su2double CConfig::GetAitkenDynMinInit ( void  )
inline

Get Aitken's maximum relaxation parameter for dynamic relaxation cases and first iteration.

Returns
Aitken's relaxation parameters.

Definition at line 1803 of file config_structure.inl.

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◆ GetAitkenStatRelax()

su2double CConfig::GetAitkenStatRelax ( void  )
inline

Get Aitken's relaxation parameter for static relaxation cases.

Returns
Aitken's relaxation parameters.

Definition at line 1799 of file config_structure.inl.

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◆ GetAnalytical_Surface()

unsigned short CConfig::GetAnalytical_Surface ( void  )
inline

Get Information about if there is an analytical definition of the surface for doing the grid adaptation.

Returns
Definition of the surfaces. NONE implies that there isn't any analytical definition and it will use and interpolation.

Definition at line 346 of file config_structure.inl.

◆ GetAoA()

su2double CConfig::GetAoA ( void  )
inline

Get the angle of attack of the body. This is the angle between a reference line on a lifting body (often the chord line of an airfoil) and the vector representing the relative motion between the lifting body and the fluid through which it is moving.

Returns
Value of the angle of attack.

Definition at line 707 of file config_structure.inl.

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◆ GetAoA_Offset()

su2double CConfig::GetAoA_Offset ( void  )
inline

Get the off set angle of attack of the body. The solution and the geometry file are able to modifity the angle of attack in the config file.

Returns
Value of the off set angle of attack.

Definition at line 721 of file config_structure.inl.

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◆ GetAoA_Sens()

su2double CConfig::GetAoA_Sens ( void  )
inline

Get the functional sensitivity with respect to changes in the angle of attack.

Returns
Value of the angle of attack.

Definition at line 725 of file config_structure.inl.

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◆ GetAoS()

su2double CConfig::GetAoS ( void  )
inline

Get the angle of sideslip of the body. It relates to the rotation of the aircraft centerline from the relative wind.

Returns
Value of the angle of sideslip.

Definition at line 719 of file config_structure.inl.

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◆ GetAoS_Offset()

su2double CConfig::GetAoS_Offset ( void  )
inline

Get the off set sideslip angle of the body. The solution and the geometry file are able to modifity the angle of attack in the config file.

Returns
Value of the off set sideslip angle.

Definition at line 723 of file config_structure.inl.

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◆ GetArrheniusCoeff()

su2double CConfig::GetArrheniusCoeff ( unsigned short  iReaction)

Provides the number of chemical reactions in the chemistry model.

Returns
: The number of chemical reactions, read from input file

◆ GetArrheniusEta()

su2double CConfig::GetArrheniusEta ( unsigned short  iReaction)

Provides the number of chemical reactions in the chemistry model.

Returns
: The number of chemical reactions, read from input file

◆ GetArrheniusTheta()

su2double CConfig::GetArrheniusTheta ( unsigned short  iReaction)

Provides the number of chemical reactions in the chemistry model.

Returns
: The number of chemical reactions, read from input file

◆ GetAverageMachLimit()

su2double CConfig::GetAverageMachLimit ( void  )
inline

Get mach limit for average massflow-based procedure .

Returns
mach limit.

Definition at line 1208 of file config_structure.inl.

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◆ GetAxisymmetric()

bool CConfig::GetAxisymmetric ( void  )
inline

Get information about the axisymmetric frame.

Returns
TRUE if there is a rotational frame; otherwise FALSE.

Definition at line 1581 of file config_structure.inl.

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◆ GetBeta_Factor()

su2double CConfig::GetBeta_Factor ( void  )
inline

Get the epsilon^2 multiplier for Beta in the incompressible preconditioner.

Returns
Value of the epsilon^2 multiplier for Beta in the incompressible preconditioner.

Definition at line 444 of file config_structure.inl.

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◆ GetBlottnerCoeff()

su2double CConfig::GetBlottnerCoeff ( unsigned short  val_Species,
unsigned short  val_Coeff 
)

Get the coefficients of the Blottner viscosity model.

Parameters
[in]val_Species- Index of the species
[in]val_Coeff- Index of the coefficient (As, Bs, Cs)
Returns
Value of the Blottner coefficient

◆ GetBody_Force()

bool CConfig::GetBody_Force ( void  )
inline

Get information about the body force.

Returns
TRUE if it uses a body force; otherwise FALSE.

Definition at line 1593 of file config_structure.inl.

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◆ GetBody_Force_Vector()

su2double * CConfig::GetBody_Force_Vector ( void  )
inline

Get a pointer to the body force vector.

Returns
A pointer to the body force vector.

Definition at line 1595 of file config_structure.inl.

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◆ GetBoolGiles()

bool CConfig::GetBoolGiles ( void  )
inline

Verify if there is any Giles Boundary Condition option specified from config file.

Returns
boolean.

Definition at line 1230 of file config_structure.inl.

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◆ GetBoolMixingPlaneInterface()

bool CConfig::GetBoolMixingPlaneInterface ( void  )
inline

Verify if there is mixing plane interface specified from config file.

Returns
boolean.

Definition at line 1216 of file config_structure.inl.

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◆ GetBoolRiemann()

bool CConfig::GetBoolRiemann ( void  )
inline

Verify if there is any Riemann Boundary Condition option specified from config file.

Returns
boolean.

Definition at line 1232 of file config_structure.inl.

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◆ GetBoolTurbMixingPlane()

bool CConfig::GetBoolTurbMixingPlane ( void  )
inline

Verify if there is mixing plane interface specified from config file.

Returns
boolean.

Definition at line 1222 of file config_structure.inl.

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◆ GetBoolTurbomachinery()

bool CConfig::GetBoolTurbomachinery ( void  )
inline

Verify if there is Turbomachinery performance option specified from config file.

Returns
boolean.

Definition at line 1218 of file config_structure.inl.

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◆ GetBoolZoneSpecific()

bool CConfig::GetBoolZoneSpecific ( void  )
inline

Verify if there are zone specific solvers entered in the config file.

Returns
boolean.

Definition at line 1220 of file config_structure.inl.

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◆ GetBreakdown_FileName()

string CConfig::GetBreakdown_FileName ( void  )
inline

Get the name of the file with the forces breakdown of the problem.

Returns
Name of the file with forces breakdown of the problem.

Definition at line 1443 of file config_structure.inl.

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◆ GetBuffet_k()

su2double CConfig::GetBuffet_k ( void  )
inline

Get the buffet sensor sharpness coefficient.

Returns
Sharpness coefficient for buffet sensor.

Definition at line 745 of file config_structure.inl.

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◆ GetBuffet_lambda()

su2double CConfig::GetBuffet_lambda ( void  )
inline

Get the buffet sensor offset parameter.

Returns
Offset parameter for buffet sensor.

Definition at line 747 of file config_structure.inl.

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◆ GetBuffet_Monitoring()

bool CConfig::GetBuffet_Monitoring ( void  )
inline

Provides the buffet monitoring information.

Returns
Buffet monitoring information, if TRUE then the code will compute the buffet sensor.

Definition at line 743 of file config_structure.inl.

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◆ GetBulk_Modulus()

su2double CConfig::GetBulk_Modulus ( void  )
inline

Get the value of the bulk modulus.

Returns
Value of the bulk modulus.

Definition at line 442 of file config_structure.inl.

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◆ GetCauchy_Elems()

unsigned short CConfig::GetCauchy_Elems ( void  )
inline

Get the number of iterations that are considered in the Cauchy convergence criteria.

Returns
Number of elements in the Cauchy criteria.

Definition at line 1499 of file config_structure.inl.

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◆ GetCauchy_Eps()

su2double CConfig::GetCauchy_Eps ( void  )
inline

Get the value of convergence criteria for the Cauchy method in the direct, adjoint or linearized problem.

Returns
Value of the convergence criteria.

Definition at line 1503 of file config_structure.inl.

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◆ GetCauchy_Func_AdjFlow()

unsigned short CConfig::GetCauchy_Func_AdjFlow ( void  )
inline

Get functional that is going to be used to evaluate the adjoint flow convergence.

Returns
Functional that is going to be used to evaluate the adjoint flow convergence.

Definition at line 1497 of file config_structure.inl.

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◆ GetCauchy_Func_Flow()

unsigned short CConfig::GetCauchy_Func_Flow ( void  )
inline

Get functional that is going to be used to evaluate the flow convergence.

Returns
Functional that is going to be used to evaluate the flow convergence.

Definition at line 1495 of file config_structure.inl.

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◆ GetCFL()

su2double CConfig::GetCFL ( unsigned short  val_mesh)
inline

Get the Courant Friedrich Levi number for each grid.

Parameters
[in]val_mesh- Index of the mesh were the CFL is applied.
Returns
CFL number for each grid.

Definition at line 755 of file config_structure.inl.

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◆ GetCFL_Adapt()

bool CConfig::GetCFL_Adapt ( void  )
inline

Get the values of the CFL adapation.

Returns
Value of CFL adapation

Definition at line 44 of file config_structure.inl.

◆ GetCFL_AdaptParam()

su2double CConfig::GetCFL_AdaptParam ( unsigned short  val_index)
inline

Get the values of the CFL adapation.

Returns
Value of CFL adapation

Definition at line 42 of file config_structure.inl.

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◆ GetCFL_Solid()

su2double CConfig::GetCFL_Solid ( void  )
inline

Get the Courant Friedrich Levi number for solid solvers.

Parameters
[in]val_mesh- Index of the mesh were the CFL is applied.
Returns
CFL number for each grid.

Definition at line 757 of file config_structure.inl.

◆ GetCFLRedCoeff_AdjTurb()

su2double CConfig::GetCFLRedCoeff_AdjTurb ( void  )
inline

Get CFL reduction factor for adjoint turbulence model.

Returns
CFL reduction factor.

Definition at line 1032 of file config_structure.inl.

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◆ GetCFLRedCoeff_Turb()

su2double CConfig::GetCFLRedCoeff_Turb ( void  )
inline

Value of the CFL reduction in LevelSet problems.

Returns
Value of the CFL reduction in LevelSet problems.

Definition at line 1575 of file config_structure.inl.

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◆ GetCharElTemp()

su2double** CConfig::GetCharElTemp ( void  )

Provides the characteristic electronic temperature for calculating e_el.

Returns
: Vector of characteristic vibrational temperatures [K]

◆ GetChargeCoeff()

su2double CConfig::GetChargeCoeff ( void  )
inline

Get the charge coefficient that is used in the poissonal potential simulation.

Returns
Value of the charge coefficient.

Definition at line 603 of file config_structure.inl.

◆ GetCharVibTemp() [1/2]

su2double CConfig::GetCharVibTemp ( unsigned short  iSpecies)

Provides the characteristic vibrational temperature for calculating e_vib.

Returns
: The number of chemical reactions, read from input file

◆ GetCharVibTemp() [2/2]

su2double* CConfig::GetCharVibTemp ( void  )

Provides the characteristic vibrational temperature for calculating e_vib.

Returns
: Vector of characteristic vibrational temperatures [K]

◆ GetCL_Target()

su2double CConfig::GetCL_Target ( void  )
inline

Value of the weight of the CD, CL, CM optimization.

Returns
Value of the weight of the CD, CL, CM optimization.

Definition at line 1569 of file config_structure.inl.

◆ GetCM_Target()

su2double CConfig::GetCM_Target ( void  )
inline

Value of the weight of the CD, CL, CM optimization.

Returns
Value of the weight of the CD, CL, CM optimization.

Definition at line 1571 of file config_structure.inl.

◆ GetCoeff_ObjChainRule()

su2double CConfig::GetCoeff_ObjChainRule ( unsigned short  iVar)
inline

Get the coefficients of the objective defined by the chain rule with primitive variables.

Author
H. Kline
Note
This objective is only applicable to gradient calculations. Objective value must be calculated using the area averaged outlet values of density, velocity, and pressure. Gradients are w.r.t density, velocity[3], and pressure. when 2D gradient w.r.t. 3rd component of velocity set to 0.

Definition at line 1280 of file config_structure.inl.

◆ GetCollective_Pitch()

su2double CConfig::GetCollective_Pitch ( void  )
inline

Collective pitch setting for rotor blades.

Returns
The specified collective pitch setting.

Definition at line 1643 of file config_structure.inl.

◆ GetComboObj()

bool CConfig::GetComboObj ( void  )

Get the flag indicating whether to comput a combined objective.

Author
H. Kline

◆ GetCompute_Average()

bool CConfig::GetCompute_Average ( void  )
inline

Get Compute Average.

Returns
YES if start computing averages

Definition at line 1961 of file config_structure.inl.

◆ GetCompute_Entropy()

bool CConfig::GetCompute_Entropy ( void  )
inline

Function to make available whether or not the entropy must be computed.

Returns
The boolean whether or not the entropy must be computed.

Definition at line 1925 of file config_structure.inl.

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◆ GetConductivity_Ref()

su2double CConfig::GetConductivity_Ref ( void  )
inline

Get the value of the reference conductivity for non-dimensionalization.

Returns
Reference conductivity for non-dimensionalization.

Definition at line 526 of file config_structure.inl.

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◆ GetConservativeInterpolation()

bool CConfig::GetConservativeInterpolation ( void  )
inline

Get option of whether to use conservative interpolation between zones.

Definition at line 1883 of file config_structure.inl.

◆ GetConsole_Output_Verb()

unsigned short CConfig::GetConsole_Output_Verb ( void  )
inline

Get the verbosity level of the console output.

Returns
Verbosity level for the console output.

Definition at line 1791 of file config_structure.inl.

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◆ GetConst_DES()

su2double CConfig::GetConst_DES ( void  )
inline

Get the DES Constant.

Returns
Value of DES constant.

Definition at line 1957 of file config_structure.inl.

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◆ GetContainerPosition()

unsigned short CConfig::GetContainerPosition ( unsigned short  val_eqsystem)

Provides the index of the solution in the container.

Parameters
[in]val_eqsystem- Equation that is being solved.
Returns
Index on the solution container.

Definition at line 7208 of file config_structure.cpp.

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◆ GetContinuous_Adjoint()

bool CConfig::GetContinuous_Adjoint ( void  )
inline

Determines if problem is adjoint.

Returns
true if Adjoint

Definition at line 290 of file config_structure.inl.

◆ GetConv_FileName()

string CConfig::GetConv_FileName ( void  )
inline

Get the name of the file with the convergence history of the problem.

Returns
Name of the file with convergence history of the problem.

Definition at line 1439 of file config_structure.inl.

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◆ GetConv_FileName_FSI()

string CConfig::GetConv_FileName_FSI ( void  )
inline

Get the name of the file with the convergence history of the problem for FSI applications.

Returns
Name of the file with convergence history of the problem.

Definition at line 1441 of file config_structure.inl.

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◆ GetConvCriteria()

unsigned short CConfig::GetConvCriteria ( void  )
inline

Obtain the kind of convergence criteria to establish the convergence of the CFD code.

Returns
Kind of convergence criteria.

Definition at line 749 of file config_structure.inl.

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◆ GetCoordFFDBox()

su2double CConfig::GetCoordFFDBox ( unsigned short  val_ffd,
unsigned short  val_index 
)
inline

Get the coordinates of the FFD corner points.

Parameters
[in]val_ffd- Index of the FFD box.
[in]val_coord- Index of the coordinate that we want to read.
Returns
Value of the coordinate.

Definition at line 767 of file config_structure.inl.

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◆ GetCriteria_FEM_ADJ()

su2double CConfig::GetCriteria_FEM_ADJ ( void  )
inline

Value of the maximum objective function for FEM elasticity adjoint (log10 scale).

Returns
Value of Res_FEM_ADJ (log10 scale).

Definition at line 1905 of file config_structure.inl.

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◆ GetCurrent_DynTime()

su2double CConfig::GetCurrent_DynTime ( void  )
inline

If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation.

Returns
Value of the time step in an unsteady simulation (non dimensional).

Definition at line 1819 of file config_structure.inl.

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◆ GetCurrent_UnstTime()

su2double CConfig::GetCurrent_UnstTime ( void  )
inline

If we are performing an unsteady simulation, this is the value of current time.

Returns
Value of the physical time in an unsteady simulation.

Definition at line 1511 of file config_structure.inl.

◆ GetCyclic_Pitch()

su2double CConfig::GetCyclic_Pitch ( void  )
inline

Cyclic pitch amplitude for rotor blades.

Returns
The specified cyclic pitch amplitude.

Definition at line 1641 of file config_structure.inl.

◆ GetDamp_Correc_Prolong()

su2double CConfig::GetDamp_Correc_Prolong ( void  )
inline

Value of the damping factor for the correction prolongation.

Returns
Value of the damping factor.

Definition at line 1539 of file config_structure.inl.

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◆ GetDamp_Engine_Exhaust()

su2double CConfig::GetDamp_Engine_Exhaust ( void  )
inline

Value of the damping factor for the engine exhaust inlet bc.

Returns
Value of the damping factor.

Definition at line 1535 of file config_structure.inl.

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◆ GetDamp_Engine_Inflow()

su2double CConfig::GetDamp_Engine_Inflow ( void  )
inline

Value of the damping factor for the engine inlet bc.

Returns
Value of the damping factor.

Definition at line 1533 of file config_structure.inl.

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◆ GetDamp_Res_Restric()

su2double CConfig::GetDamp_Res_Restric ( void  )
inline

Value of the damping factor for the residual restriction.

Returns
Value of the damping factor.

Definition at line 1537 of file config_structure.inl.

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◆ GetDamper_Constant()

su2double CConfig::GetDamper_Constant ( string  val_index)

Get the constant value at a damper boundary.

Parameters
[in]val_index- Index corresponding to the load boundary.
Returns
The damper constant.

Definition at line 8345 of file config_structure.cpp.

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◆ GetdCD_dCL()

su2double CConfig::GetdCD_dCL ( void  )
inline

Value of the weight of the CD, CL, CM optimization.

Returns
Value of the weight of the CD, CL, CM optimization.

Definition at line 1545 of file config_structure.inl.

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◆ GetdCD_dCMy()

su2double CConfig::GetdCD_dCMy ( void  )
inline

Value of the weight of the CD, CL, CM optimization.

Returns
Value of the weight of the CD, CL, CM optimization.

Definition at line 1565 of file config_structure.inl.

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◆ GetdCL_dAlpha()

su2double CConfig::GetdCL_dAlpha ( void  )
inline

Get the value for the lift curve slope for fixed CL mode.

Returns
Lift curve slope for fixed CL mode.

Definition at line 1759 of file config_structure.inl.

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◆ GetdCM_diH()

su2double CConfig::GetdCM_diH ( void  )
inline

Get the value of the damping coefficient for fixed CL mode.

Returns
Damping coefficient for fixed CL mode.

Definition at line 1761 of file config_structure.inl.

◆ GetdCMx_dCL()

su2double CConfig::GetdCMx_dCL ( void  )
inline

Value of the weight of the CD, CL, CM optimization.

Returns
Value of the weight of the CD, CL, CM optimization.

Definition at line 1547 of file config_structure.inl.

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◆ GetdCMy_dCL()

su2double CConfig::GetdCMy_dCL ( void  )
inline

Value of the weight of the CD, CL, CM optimization.

Returns
Value of the weight of the CD, CL, CM optimization.

Definition at line 1549 of file config_structure.inl.

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◆ GetdCMz_dCL()

su2double CConfig::GetdCMz_dCL ( void  )
inline

Value of the weight of the CD, CL, CM optimization.

Returns
Value of the weight of the CD, CL, CM optimization.

Definition at line 1551 of file config_structure.inl.

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◆ GetDE_Effects()

bool CConfig::GetDE_Effects ( void  )
inline

Decide whether to apply DE effects to the model.

Returns
TRUE if the DE effects are to be applied, FALSE otherwise.

Definition at line 366 of file config_structure.inl.

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◆ GetDE_Predicted()

bool CConfig::GetDE_Predicted ( void  )

Decide whether to predict the DE effects for the next time step.

Returns
TRUE if the DE effects are to be applied, FALSE otherwise.

◆ GetDeadLoad()

bool CConfig::GetDeadLoad ( void  )
inline

Decide whether to apply dead loads to the model.

Returns
TRUE if the dead loads are to be applied, FALSE otherwise.

Definition at line 1805 of file config_structure.inl.

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◆ GetDebugMode()

bool CConfig::GetDebugMode ( void  )

Get information about the axisymmetric frame.

Returns
TRUE if there is a rotational frame; otherwise FALSE.

◆ GetDeform_Coeff()

su2double CConfig::GetDeform_Coeff ( void  )
inline

Get factor to multiply smallest volume for deform tolerance.

Returns
Factor to multiply smallest volume for deform tolerance.

Definition at line 1042 of file config_structure.inl.

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◆ GetDeform_ElasticityMod()

su2double CConfig::GetDeform_ElasticityMod ( void  )
inline

Get Young's modulus for deformation (constant stiffness deformation)

Definition at line 1046 of file config_structure.inl.

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◆ GetDeform_Limit()

su2double CConfig::GetDeform_Limit ( void  )
inline

Get limit for the volumetric deformation.

Returns
Distance to the surface to be deformed.

Definition at line 1044 of file config_structure.inl.

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◆ GetDeform_Linear_Solver_Error()

su2double CConfig::GetDeform_Linear_Solver_Error ( void  )
inline

Get min error of the linear solver for the implicit formulation.

Returns
Min error of the linear solver for the implicit formulation.

Definition at line 992 of file config_structure.inl.

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◆ GetDeform_Linear_Solver_Iter()

unsigned long CConfig::GetDeform_Linear_Solver_Iter ( void  )
inline

Get max number of iterations of the linear solver for the implicit formulation.

Returns
Max number of iterations of the linear solver for the implicit formulation.

Definition at line 996 of file config_structure.inl.

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◆ GetDeform_Output()

bool CConfig::GetDeform_Output ( void  )
inline

Get information about writing grid deformation residuals to the console.

Returns
TRUE means that grid deformation residuals will be written to the console.

Definition at line 1038 of file config_structure.inl.

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◆ GetDeform_PoissonRatio()

su2double CConfig::GetDeform_PoissonRatio ( void  )
inline

Get Poisson's ratio for deformation (constant stiffness deformation) .

Definition at line 1048 of file config_structure.inl.

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◆ GetDeform_Stiffness_Type()

unsigned short CConfig::GetDeform_Stiffness_Type ( void  )
inline

Get the type of stiffness to impose for FEA mesh deformation.

Returns
type of stiffness to impose for FEA mesh deformation.

Definition at line 1050 of file config_structure.inl.

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◆ GetDeform_Tol_Factor()

su2double CConfig::GetDeform_Tol_Factor ( void  )
inline

Get factor to multiply smallest volume for deform tolerance.

Returns
Factor to multiply smallest volume for deform tolerance.

Definition at line 1040 of file config_structure.inl.

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◆ GetDegreeFFDBox()

unsigned short CConfig::GetDegreeFFDBox ( unsigned short  val_ffd,
unsigned short  val_index 
)
inline

Get the degree of the FFD corner points.

Parameters
[in]val_ffd- Index of the FFD box.
[in]val_degree- Index (I,J,K) to obtain the degree.
Returns
Value of the degree in a particular direction.

Definition at line 769 of file config_structure.inl.

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◆ GetDelta_DynTime()

su2double CConfig::GetDelta_DynTime ( void  )
inline

If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation.

Returns
Value of the time step in an unsteady simulation (non dimensional).

Definition at line 1815 of file config_structure.inl.

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◆ GetDelta_UnstTime()

su2double CConfig::GetDelta_UnstTime ( void  )
inline

If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation.

Returns
Value of the time step in an unsteady simulation.

Definition at line 1509 of file config_structure.inl.

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◆ GetDelta_UnstTimeND()

su2double CConfig::GetDelta_UnstTimeND ( void  )
inline

If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation.

Returns
Value of the time step in an unsteady simulation (non dimensional).

Definition at line 1505 of file config_structure.inl.

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◆ GetDensity_FreeStream()

su2double CConfig::GetDensity_FreeStream ( void  )
inline

Get the value of the frestream temperature.

Returns
Freestream temperature.

Definition at line 490 of file config_structure.inl.

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◆ GetDensity_FreeStreamND()

su2double CConfig::GetDensity_FreeStreamND ( void  )
inline

Get the value of the non-dimensionalized freestream density.

Returns
Non-dimensionalized freestream density.

Definition at line 542 of file config_structure.inl.

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◆ GetDensity_Ref()

su2double CConfig::GetDensity_Ref ( void  )
inline

Get the value of the reference density for non-dimensionalization.

Returns
Reference density for non-dimensionalization.

Definition at line 516 of file config_structure.inl.

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◆ GetDensity_Solid()

su2double CConfig::GetDensity_Solid ( void  )
inline

Get the value of the solid density.

Returns
Solid density.

Definition at line 492 of file config_structure.inl.

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◆ GetDesign_Variable()

unsigned short CConfig::GetDesign_Variable ( unsigned short  val_dv)
inline

Obtain the kind of design variable.

Parameters
[in]val_dv- Number of the design variable that we want to read.
Returns
Design variable identification.

Definition at line 737 of file config_structure.inl.

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◆ GetDirectDiff()

unsigned short CConfig::GetDirectDiff ( )
inline

Get the direct differentation method.

Returns
direct differentiation method.

Definition at line 1909 of file config_structure.inl.

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◆ GetDirichlet_Boundary()

bool CConfig::GetDirichlet_Boundary ( string  val_index)

Get whether this is a Dirichlet or a Neumann boundary.

Parameters
[in]val_index- Index corresponding to the Dirichlet boundary.
Returns
Yes or No.

Definition at line 7610 of file config_structure.cpp.

◆ GetDirichlet_Value()

su2double CConfig::GetDirichlet_Value ( string  val_index)

Get the fixed value at the Dirichlet boundary.

Parameters
[in]val_index- Index corresponding to the Dirichlet boundary.
Returns
The total temperature.

Definition at line 7603 of file config_structure.cpp.

◆ GetDiscard_InFiles()

bool CConfig::GetDiscard_InFiles ( void  )
inline

Get information about whether to use fixed CL mode.

Returns
TRUE if fixed CL mode is active; otherwise FALSE.

Definition at line 1755 of file config_structure.inl.

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◆ GetDiscrete_Adjoint()

bool CConfig::GetDiscrete_Adjoint ( void  )
inline

Get the indicator whether we are solving an discrete adjoint problem.

Returns
the discrete adjoint indicator.

Definition at line 1911 of file config_structure.inl.

◆ GetDisp_Dir()

su2double * CConfig::GetDisp_Dir ( string  val_index)

Get the force direction at a loaded boundary in cartesian coordinates.

Parameters
[in]val_index- Index corresponding to the load boundary.
Returns
The load direction.

Definition at line 8387 of file config_structure.cpp.

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◆ GetDisp_Dir_Multiplier()

su2double CConfig::GetDisp_Dir_Multiplier ( string  val_index)

Get the force multiplier at a load boundary in cartesian coordinates.

Parameters
[in]val_index- Index corresponding to the load boundary.
Returns
The load multiplier.

Definition at line 8373 of file config_structure.cpp.

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◆ GetDisp_Dir_Value()

su2double CConfig::GetDisp_Dir_Value ( string  val_index)

Get the force value at a load boundary defined in cartesian coordinates.

Parameters
[in]val_index- Index corresponding to the load boundary.
Returns
The load value.

Definition at line 8366 of file config_structure.cpp.

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◆ GetDispl_Value()

su2double CConfig::GetDispl_Value ( string  val_index)

Get the displacement value at an displacement boundary.

Parameters
[in]val_index- Index corresponding to the displacement boundary.
Returns
The displacement value.

Definition at line 8331 of file config_structure.cpp.

◆ GetDissociationPot()

su2double* CConfig::GetDissociationPot ( void  )

Dissociation potential of species.

Returns
: Dissociation potential.

◆ GetDistortionRack()

su2double * CConfig::GetDistortionRack ( void  )
inline

Get the the coordinates where of the box where a subsonic region is imposed.

Returns
Coordinates where of the box where the grid is going to be a subsonic region.

Definition at line 344 of file config_structure.inl.

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◆ GetdNetThrust_dBCThrust()

su2double CConfig::GetdNetThrust_dBCThrust ( void  )
inline

Get the value of the damping coefficient for fixed CL mode.

Returns
Damping coefficient for fixed CL mode.

Definition at line 1781 of file config_structure.inl.

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◆ GetDomainVolume()

su2double CConfig::GetDomainVolume ( void  )
inline

Get the volume of the whole domain using the fine grid, this value is common for all the grids in the multigrid method.

Returns
Volume of the whole domain.

Definition at line 424 of file config_structure.inl.

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◆ GetDualVol_Power()

su2double CConfig::GetDualVol_Power ( void  )
inline

Get the power of the dual volume in the grid adaptation sensor.

Returns
Power of the dual volume in the grid adaptation sensor.

Definition at line 350 of file config_structure.inl.

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◆ GetDV_FEA()

unsigned short CConfig::GetDV_FEA ( void  )
inline

Get the kind of design variable for FEA.

Returns
Value of the DE voltage.

Definition at line 376 of file config_structure.inl.

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◆ GetDV_Filename()

string CConfig::GetDV_Filename ( void  )
inline

Get name of the arbitrary mesh motion input file.

Returns
File name of the arbitrary mesh motion input file.

Definition at line 1645 of file config_structure.inl.

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◆ GetDV_Value()

su2double CConfig::GetDV_Value ( unsigned short  val_dv,
unsigned short  val_val = 0 
)
inline

Value of the design variable step, we use this value in design problems.

Parameters
[in]val_dv- Number of the design variable that we want to read.
[in]val_value- Value of the design variable that we want to read.
Returns
Design variable step.

Definition at line 1525 of file config_structure.inl.

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◆ GetDyn_nIntIter()

unsigned long CConfig::GetDyn_nIntIter ( void  )
inline

Get the number of internal iterations for the Newton-Raphson Method in nonlinear structural applications.

Returns
Number of internal iterations.

Definition at line 318 of file config_structure.inl.

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◆ GetDyn_RestartIter()

long CConfig::GetDyn_RestartIter ( void  )
inline

Get the restart iteration number for dynamic structural simulations.

Returns
Restart iteration number for dynamic structural simulations.

Definition at line 328 of file config_structure.inl.

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◆ GetDynamic_Analysis()

unsigned short CConfig::GetDynamic_Analysis ( void  )
inline

Provides information about the time integration of the structural analysis, and change the write in the output files information about the iteration.

Returns
The kind of time integration: Static or dynamic analysis

Definition at line 1813 of file config_structure.inl.

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◆ GetDynamic_LoadTransfer()

unsigned short CConfig::GetDynamic_LoadTransfer ( void  )
inline

Get the kind of load transfer method we want to use for dynamic problems.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of transfer method for multiphysics problems

Definition at line 1907 of file config_structure.inl.

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◆ GetEA_IntLimit()

su2double CConfig::GetEA_IntLimit ( unsigned short  index)
inline

Get the integration limits for the equivalent area computation.

Parameters
[in]index- 0 means x_min, and 1 means x_max.
Returns
Integration limits for the equivalent area computation.

Definition at line 332 of file config_structure.inl.

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◆ GetEA_ScaleFactor()

su2double CConfig::GetEA_ScaleFactor ( void  )
inline

Get the integration limits for the equivalent area computation.

Parameters
[in]index- 0 means x_min, and 1 means x_max.
Returns
Integration limits for the equivalent area computation.

Definition at line 334 of file config_structure.inl.

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◆ GetElas2D_Formulation()

unsigned short CConfig::GetElas2D_Formulation ( void  )
inline

Formulation for 2D elasticity (plane stress - strain)

Returns
Flag to 2D elasticity model.

Definition at line 390 of file config_structure.inl.

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◆ GetElasticyMod()

su2double CConfig::GetElasticyMod ( unsigned short  id_val)
inline

Get the Young's modulus of elasticity.

Returns
Value of the Young's modulus of elasticity.

Definition at line 364 of file config_structure.inl.

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◆ GetElDegeneracy()

su2double** CConfig::GetElDegeneracy ( void  )

Provides the degeneracy of electron states for calculating e_el.

Returns
: Vector of characteristic vibrational temperatures [K]

◆ GetElectric_Constant()

su2double CConfig::GetElectric_Constant ( unsigned short  iVar)
inline

Get the value of the DE modulus.

Returns
Value of the DE modulus.

Definition at line 370 of file config_structure.inl.

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◆ GetEnergy_Equation()

bool CConfig::GetEnergy_Equation ( void  )
inline

Flag for whether to solve the energy equation for incompressible flows.

Returns
Flag for energy equation

Definition at line 862 of file config_structure.inl.

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◆ GetEnergy_FreeStream()

su2double CConfig::GetEnergy_FreeStream ( void  )
inline

Get the value of the frestream temperature.

Returns
Freestream temperature.

Definition at line 486 of file config_structure.inl.

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◆ GetEnergy_FreeStreamND()

su2double CConfig::GetEnergy_FreeStreamND ( void  )
inline

Get the value of the non-dimensionalized freestream energy.

Returns
Non-dimensionalized freestream energy.

Definition at line 548 of file config_structure.inl.

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◆ GetEnergy_Ref()

su2double CConfig::GetEnergy_Ref ( void  )
inline

Get the value of the reference pressure for non-dimensionalization.

Returns
Reference pressure for non-dimensionalization.

Definition at line 520 of file config_structure.inl.

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◆ GetEngine_Area()

su2double CConfig::GetEngine_Area ( unsigned short  val_imarker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_imarker- Index corresponding to a particular engine boundary.
Returns
The outlet pressure.

Definition at line 276 of file config_structure.inl.

◆ GetEngine_Force()

su2double CConfig::GetEngine_Force ( unsigned short  val_imarker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_imarker- Index corresponding to a particular engine boundary.
Returns
The outlet pressure.

Definition at line 268 of file config_structure.inl.

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◆ GetEngine_GrossThrust()

su2double CConfig::GetEngine_GrossThrust ( unsigned short  val_imarker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_imarker- Index corresponding to a particular engine boundary.
Returns
The outlet pressure.

Definition at line 274 of file config_structure.inl.

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◆ GetEngine_HalfModel()

bool CConfig::GetEngine_HalfModel ( void  )
inline

Only halg of the engine is in the compputational grid.

Returns
TRUE if the engine is complete; otherwise FALSE.

Definition at line 1521 of file config_structure.inl.

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◆ GetEngine_Mach()

su2double CConfig::GetEngine_Mach ( unsigned short  val_imarker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_imarker- Index corresponding to a particular engine boundary.
Returns
The outlet pressure.

Definition at line 266 of file config_structure.inl.

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◆ GetEngine_NetThrust()

su2double CConfig::GetEngine_NetThrust ( unsigned short  val_imarker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_imarker- Index corresponding to a particular engine boundary.
Returns
The outlet pressure.

Definition at line 272 of file config_structure.inl.

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◆ GetEngine_Power()

su2double CConfig::GetEngine_Power ( unsigned short  val_imarker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_imarker- Index corresponding to a particular engine boundary.
Returns
The outlet pressure.

Definition at line 270 of file config_structure.inl.

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◆ GetEngineInflow_Target()

su2double CConfig::GetEngineInflow_Target ( string  val_marker)

Get the target (pressure, massflow, etc) at an engine inflow boundary.

Parameters
[in]val_index- Index corresponding to the engine inflow boundary.
Returns
Target (pressure, massflow, etc) .

Definition at line 8086 of file config_structure.cpp.

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◆ GetEnthalpy_Formation() [1/2]

su2double CConfig::GetEnthalpy_Formation ( unsigned short  iSpecies)

Provides the formation enthalpy of the specified species at standard conditions.

Returns
: Enthalpy of formation

◆ GetEnthalpy_Formation() [2/2]

su2double* CConfig::GetEnthalpy_Formation ( void  )

Provides the formation enthalpy of the specified species at standard conditions.

Returns
: Enthalpy of formation

◆ GetEntropyFix_Coeff()

su2double CConfig::GetEntropyFix_Coeff ( void  )
inline

Get the entropy fix.

Returns
Vaule of the entropy fix.

Definition at line 1028 of file config_structure.inl.

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◆ GetEquivArea()

bool CConfig::GetEquivArea ( void  )
inline

Information about computing and plotting the equivalent area distribution.

Returns
TRUE or FALSE depending if we are computing the equivalent area.

Definition at line 1294 of file config_structure.inl.

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◆ GetEulerPersson()

bool CConfig::GetEulerPersson ( void  )
inline

Get boolean for using Persson's shock capturing method in Euler flow DG-FEM.

Returns
Boolean for using Persson's shock capturing method in Euler flow DG-FEM

Definition at line 1867 of file config_structure.inl.

◆ GetEval_dOF_dCX()

bool CConfig::GetEval_dOF_dCX ( void  )
inline

Get information about whether to use fixed CL mode.

Returns
TRUE if fixed CL mode is active; otherwise FALSE.

Definition at line 1753 of file config_structure.inl.

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◆ GetExhaust_Force()

su2double CConfig::GetExhaust_Force ( string  val_marker)

Get the force balance at an engine exhaust boundary.

Parameters
[in]val_marker- Name of the boundary.
Returns
Force balance.

Definition at line 8205 of file config_structure.cpp.

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◆ GetExhaust_GrossThrust()

su2double CConfig::GetExhaust_GrossThrust ( string  val_marker)

Get the gross thrust at an engine exhaust boundary.

Parameters
[in]val_marker- Name of the boundary.
Returns
Gross thrust.

Definition at line 8198 of file config_structure.cpp.

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◆ GetExhaust_MassFlow()

su2double CConfig::GetExhaust_MassFlow ( string  val_marker)

Get the massflow at an engine exhaust boundary.

Parameters
[in]val_marker- Name of the boundary.
Returns
The engine exhaust massflow.

Definition at line 8177 of file config_structure.cpp.

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◆ GetExhaust_Power()

su2double CConfig::GetExhaust_Power ( string  val_marker)

Get the power at an engine exhaust boundary.

Parameters
[in]val_marker- Name of the boundary.
Returns
Power.

Definition at line 8212 of file config_structure.cpp.

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◆ GetExhaust_Pressure()

su2double CConfig::GetExhaust_Pressure ( string  val_marker)

Get the back pressure (static) at an engine exhaust boundary.

Parameters
[in]val_marker- Name of the boundary.
Returns
The engine exhaust pressure.

Definition at line 8163 of file config_structure.cpp.

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◆ GetExhaust_Pressure_Target()

su2double CConfig::GetExhaust_Pressure_Target ( string  val_index)

Get the total pressure at an nacelle boundary.

Parameters
[in]val_index- Index corresponding to the inlet boundary.
Returns
The total pressure.

Definition at line 7628 of file config_structure.cpp.

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◆ GetExhaust_Temperature()

su2double CConfig::GetExhaust_Temperature ( string  val_marker)

Get the temperature (static) at an engine exhaust boundary.

Parameters
[in]val_marker- Name of the boundary.
Returns
The engine exhaust temperature.

Definition at line 8170 of file config_structure.cpp.

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◆ GetExhaust_Temperature_Target()

su2double CConfig::GetExhaust_Temperature_Target ( string  val_index)

Get the total temperature at a nacelle boundary.

Parameters
[in]val_index- Index corresponding to the inlet boundary.
Returns
The total temperature.

Definition at line 7621 of file config_structure.cpp.

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◆ GetExhaust_TotalPressure()

su2double CConfig::GetExhaust_TotalPressure ( string  val_marker)

Get the total pressure at an engine exhaust boundary.

Parameters
[in]val_marker- Name of the boundary.
Returns
The engine exhaust total pressure.

Definition at line 8184 of file config_structure.cpp.

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◆ GetExhaust_TotalTemperature()

su2double CConfig::GetExhaust_TotalTemperature ( string  val_marker)

Get the total temperature at an engine exhaust boundary.

Parameters
[in]val_marker- Name of the boundary.
Returns
The total temperature.

Definition at line 8191 of file config_structure.cpp.

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◆ GetExtIter()

unsigned long CConfig::GetExtIter ( void  )
inline

Get the current external iteration number.

Returns
Current external iteration.

Definition at line 308 of file config_structure.inl.

◆ GetExtIter_OffSet()

unsigned long CConfig::GetExtIter_OffSet ( void  )
inline

Get the current internal iteration number.

Returns
Current external iteration.

Definition at line 310 of file config_structure.inl.

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◆ GetExtraHeatOutputZone()

long CConfig::GetExtraHeatOutputZone ( void  )
inline

Heat solver zone with extra screen output.

Returns
Heat solver zone with extra screen output.

Definition at line 354 of file config_structure.inl.

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◆ GetExtraOutput()

bool CConfig::GetExtraOutput ( void  )
inline

Creates a tecplot file to visualize the partition made by the DDC software.

Returns
TRUE if the partition is going to be plotted; otherwise FALSE.

Definition at line 352 of file config_structure.inl.

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◆ GetExtraRelFacGiles()

su2double CConfig::GetExtraRelFacGiles ( unsigned short  iCoeff)
inline

Get extra relaxation factor coefficients for the Giels BC.

Returns
mixedout coefficient.

Definition at line 1206 of file config_structure.inl.

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◆ GetFan_Poly_Eff()

su2double CConfig::GetFan_Poly_Eff ( void  )
inline

Get the value of the reference viscosity for non-dimensionalization.

Returns
Reference viscosity for non-dimensionalization.

Definition at line 530 of file config_structure.inl.

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◆ GetFEA_FileName()

string CConfig::GetFEA_FileName ( void  )
inline

Get the name of the file with the element properties for structural problems.

Returns
Name of the file with the element properties of the structural problem.

Definition at line 414 of file config_structure.inl.

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◆ GetFFD_Axis()

su2double CConfig::GetFFD_Axis ( unsigned short  val_var)
inline

Get the value of the vector that connects the cartesian axis with a sherical or cylindrical one.

Returns
Coordinate of the Axis.

Definition at line 440 of file config_structure.inl.

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◆ GetFFD_Blending()

unsigned short CConfig::GetFFD_Blending ( void  )
inline

Get the kind of FFD Blending function.

Returns
Kind of FFD Blending function.

Definition at line 1939 of file config_structure.inl.

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◆ GetFFD_BSplineOrder()

su2double * CConfig::GetFFD_BSplineOrder ( )
inline

Get the kind BSpline Order in i,j,k direction.

Returns
The kind BSpline Order in i,j,k direction.

Definition at line 1941 of file config_structure.inl.

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◆ GetFFD_Continuity()

unsigned short CConfig::GetFFD_Continuity ( void  )
inline

Get the required continuity level at the surface intersection with the FFD.

Returns
Continuity level at the surface intersection.

Definition at line 781 of file config_structure.inl.

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◆ GetFFD_CoordSystem()

unsigned short CConfig::GetFFD_CoordSystem ( void  )
inline

Get the coordinate system that we are going to use to define the FFD.

Returns
Coordinate system (cartesian, spherical, etc).

Definition at line 783 of file config_structure.inl.

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◆ GetFFD_Fix_IDir()

short CConfig::GetFFD_Fix_IDir ( unsigned short  val_index)
inline

plane of the FFD (I axis) that should be fixed.

Parameters
[in]val_index- Index of the arrray with all the planes in the I direction that should be fixed.
Returns
Index of the plane that is going to be freeze.

Definition at line 813 of file config_structure.inl.

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◆ GetFFD_Fix_JDir()

short CConfig::GetFFD_Fix_JDir ( unsigned short  val_index)
inline

plane of the FFD (J axis) that should be fixed.

Parameters
[in]val_index- Index of the arrray with all the planes in the J direction that should be fixed.
Returns
Index of the plane that is going to be freeze.

Definition at line 815 of file config_structure.inl.

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◆ GetFFD_Fix_KDir()

short CConfig::GetFFD_Fix_KDir ( unsigned short  val_index)
inline

plane of the FFD (K axis) that should be fixed.

Parameters
[in]val_index- Index of the arrray with all the planes in the K direction that should be fixed.
Returns
Index of the plane that is going to be freeze.

Definition at line 817 of file config_structure.inl.

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◆ GetFFD_Symmetry_Plane()

bool CConfig::GetFFD_Symmetry_Plane ( void  )
inline

Define the FFD box with a symetry plane.

Returns
TRUE if there is a symmetry plane in the FFD; otherwise FALSE.

Definition at line 1056 of file config_structure.inl.

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◆ GetFFD_Tol()

su2double CConfig::GetFFD_Tol ( void  )
inline

Get the tolerance of the point inversion algorithm.

Returns
Tolerance of the point inversion algorithm.

Definition at line 1737 of file config_structure.inl.

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◆ GetFFDTag()

string CConfig::GetFFDTag ( unsigned short  val_dv)
inline

Get the FFD Tag of a particular design variable.

Parameters
[in]val_dv- Number of the design variable that we want to read.
Returns
Name of the FFD box.

Definition at line 771 of file config_structure.inl.

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◆ GetFinalOutletPressure()

su2double CConfig::GetFinalOutletPressure ( void  )
inline

Get final Outlet Pressure value for the ramp.

Returns
final Outlet Pressure value.

Definition at line 1196 of file config_structure.inl.

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◆ GetFinalRotation_Rate_Z()

su2double CConfig::GetFinalRotation_Rate_Z ( unsigned short  val_iZone)
inline

Get the angular velocity of the mesh about the z-axis.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Angular velocity of the mesh about the z-axis.

Definition at line 936 of file config_structure.inl.

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◆ GetFinestMesh()

unsigned short CConfig::GetFinestMesh ( void  )
inline

Get the index of the finest grid.

Returns
Index of the finest grid in a multigrid strategy, this is 0 unless we are performing a Full multigrid.

Definition at line 731 of file config_structure.inl.

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◆ GetFixAzimuthalLine()

su2double CConfig::GetFixAzimuthalLine ( void  )
inline

Value of the azimuthal line to fix due to a misalignments of the nearfield.

Returns
Azimuthal line to fix due to a misalignments of the nearfield.

Definition at line 1573 of file config_structure.inl.

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◆ GetFixed_CL_Mode()

bool CConfig::GetFixed_CL_Mode ( void  )
inline

Get information about whether to use fixed CL mode.

Returns
TRUE if fixed CL mode is active; otherwise FALSE.

Definition at line 1749 of file config_structure.inl.

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◆ GetFixed_CM_Mode()

bool CConfig::GetFixed_CM_Mode ( void  )
inline

Get information about whether to use fixed CL mode.

Returns
TRUE if fixed CL mode is active; otherwise FALSE.

Definition at line 1751 of file config_structure.inl.

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◆ GetFlow_FileName()

string CConfig::GetFlow_FileName ( void  )
inline

Get the name of the file with the flow variables.

Returns
Name of the file with the primitive variables.

Definition at line 1453 of file config_structure.inl.

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◆ GetFlowAngleIn_BC()

su2double CConfig::GetFlowAngleIn_BC ( )

Get the inlet flow angle imposed as BC for internal flow.

Returns
inlet flow angle

Definition at line 7872 of file config_structure.cpp.

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◆ GetFlowLoad_Value()

su2double CConfig::GetFlowLoad_Value ( string  val_index)

Get the force value at an load boundary.

Parameters
[in]val_index- Index corresponding to the load boundary.
Returns
The load value.

Definition at line 8415 of file config_structure.cpp.

◆ GetForce_Ref()

su2double CConfig::GetForce_Ref ( void  )
inline

Get the value of the reference force for non-dimensionalization.

Returns
Reference force for non-dimensionalization.

Definition at line 534 of file config_structure.inl.

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◆ GetFreeStreamTurboNormal()

su2double * CConfig::GetFreeStreamTurboNormal ( void  )
inline

Set freestream turbonormal for initializing solution.

Definition at line 1180 of file config_structure.inl.

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◆ GetFroude()

su2double CConfig::GetFroude ( void  )
inline

Get the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 613 of file config_structure.inl.

◆ GetFrozen_Limiter_Disc()

bool CConfig::GetFrozen_Limiter_Disc ( void  )
inline

Provides information about the way in which the limiter will be treated by the disc. adjoint method.

Returns
FALSE means that the limiter computation is included.

Definition at line 1611 of file config_structure.inl.

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◆ GetFrozen_Visc_Cont()

bool CConfig::GetFrozen_Visc_Cont ( void  )
inline

Provides information about the way in which the turbulence will be treated by the cont. adjoint method.

Returns
FALSE means that the adjoint turbulence equations will be used.

Definition at line 1607 of file config_structure.inl.

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◆ GetFrozen_Visc_Disc()

bool CConfig::GetFrozen_Visc_Disc ( void  )
inline

Provides information about the way in which the turbulence will be treated by the disc. adjoint method.

Returns
FALSE means that the adjoint turbulence equations will be used.

Definition at line 1609 of file config_structure.inl.

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◆ GetFSI_Simulation()

bool CConfig::GetFSI_Simulation ( void  )
inline

Check if the simulation we are running is a FSI simulation.

Returns
Value of the physical time in an unsteady simulation.

Definition at line 1871 of file config_structure.inl.

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◆ GetFSIIter()

unsigned long CConfig::GetFSIIter ( void  )
inline

Get the current FSI iteration number.

Returns
Current FSI iteration.

Definition at line 312 of file config_structure.inl.

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◆ GetGamma()

su2double CConfig::GetGamma ( void  )
inline

Get the value of the Gamma of fluid (ratio of specific heats).

Returns
Value of the constant: Gamma

Definition at line 436 of file config_structure.inl.

◆ GetGas_Constant()

su2double CConfig::GetGas_Constant ( void  )
inline

Get the value of specific gas constant.

Returns
Value of the constant: Gamma

Definition at line 446 of file config_structure.inl.

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◆ GetGas_Constant_Ref()

su2double CConfig::GetGas_Constant_Ref ( void  )
inline

Get the reference value for the specific gas constant.

Returns
Reference value for the specific gas constant.

Definition at line 482 of file config_structure.inl.

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◆ GetGas_ConstantND()

su2double CConfig::GetGas_ConstantND ( void  )
inline

Get the value of specific gas constant.

Returns
Value of the constant: Gamma

Definition at line 448 of file config_structure.inl.

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◆ GetGeo_Description()

unsigned short CConfig::GetGeo_Description ( void  )
inline

Get Description of the geometry to be analyzed.

Definition at line 348 of file config_structure.inl.

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◆ GetGeo_Waterline_Location()

su2double CConfig::GetGeo_Waterline_Location ( void  )
inline

Get the location of the waterline.

Returns
Z location of the waterline.

Definition at line 1268 of file config_structure.inl.

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◆ GetGeometricConditions()

unsigned short CConfig::GetGeometricConditions ( void  )
inline

Geometric conditions for the structural solver.

Returns
Small or large deformation structural analysis.

Definition at line 406 of file config_structure.inl.

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◆ GetGeometryMode()

unsigned short CConfig::GetGeometryMode ( void  )
inline

Get the king of evaluation in the geometrical module.

Returns
0 or 1 depending of we are dealing with a V or W cycle.

Definition at line 753 of file config_structure.inl.

◆ GetGiles_FlowDir()

su2double * CConfig::GetGiles_FlowDir ( string  val_marker)

Get the Flowdir for the Giles BC.

Parameters
[in]val_marker- Index corresponding to the Giles BC.
Returns
The Flowdir

Definition at line 7769 of file config_structure.cpp.

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◆ GetGiles_RelaxFactorAverage()

su2double CConfig::GetGiles_RelaxFactorAverage ( string  val_marker)

Get the relax factor for the average component for the Giles BC.

Parameters
[in]val_marker- Index corresponding to the Giles BC.
Returns
The relax factor for the average component

Definition at line 7755 of file config_structure.cpp.

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◆ GetGiles_RelaxFactorFourier()

su2double CConfig::GetGiles_RelaxFactorFourier ( string  val_marker)

Get the relax factor for the fourier component for the Giles BC.

Parameters
[in]val_marker- Index corresponding to the Giles BC.
Returns
The relax factor for the fourier component

Definition at line 7762 of file config_structure.cpp.

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◆ GetGiles_Var1()

su2double CConfig::GetGiles_Var1 ( string  val_marker)

Get the var 1 for the Giels BC.

Parameters
[in]val_marker- Index corresponding to the Giles BC.
Returns
The var1

Definition at line 7734 of file config_structure.cpp.

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◆ GetGiles_Var2()

su2double CConfig::GetGiles_Var2 ( string  val_marker)

Get the var 2 for the Giles boundary.

Parameters
[in]val_marker- Index corresponding to the Giles BC.
Returns
The var2

Definition at line 7748 of file config_structure.cpp.

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◆ GetGravityForce()

bool CConfig::GetGravityForce ( void  )
inline

Get information about the gravity force.

Returns
TRUE if it uses the gravity force; otherwise FALSE.

Definition at line 1591 of file config_structure.inl.

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◆ GetGrid_Movement()

bool CConfig::GetGrid_Movement ( void  )
inline

Get information about the grid movement.

Returns
TRUE if there is a grid movement; otherwise FALSE.

Definition at line 1577 of file config_structure.inl.

◆ GetGridDef_Linear_Iter()

unsigned long CConfig::GetGridDef_Linear_Iter ( void  )
inline

Get the number of linear smoothing iterations for mesh deformation.

Returns
Number of linear smoothing iterations for mesh deformation.

Definition at line 1034 of file config_structure.inl.

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◆ GetGridDef_Nonlinear_Iter()

unsigned long CConfig::GetGridDef_Nonlinear_Iter ( void  )
inline

Get the number of nonlinear increments for mesh deformation.

Returns
Number of nonlinear increments for mesh deformation.

Definition at line 1036 of file config_structure.inl.

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◆ GetGust_Ampl()

su2double CConfig::GetGust_Ampl ( void  )
inline

Value of the gust amplitude.

Definition at line 1729 of file config_structure.inl.

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◆ GetGust_Begin_Loc()

su2double CConfig::GetGust_Begin_Loc ( void  )
inline

Value of the location ath which the gust begins.

Definition at line 1733 of file config_structure.inl.

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◆ GetGust_Begin_Time()

su2double CConfig::GetGust_Begin_Time ( void  )
inline

Value of the time at which to begin the gust.

Definition at line 1731 of file config_structure.inl.

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◆ GetGust_Dir()

unsigned short CConfig::GetGust_Dir ( void  )
inline

Get the gust direction.

Returns
the gust direction.

Definition at line 1723 of file config_structure.inl.

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◆ GetGust_Periods()

su2double CConfig::GetGust_Periods ( void  )
inline

Value of the number of gust periods.

Definition at line 1727 of file config_structure.inl.

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◆ GetGust_Type()

unsigned short CConfig::GetGust_Type ( void  )
inline

Get the type of gust to simulate.

Returns
type of gust to use for the simulation.

Definition at line 1721 of file config_structure.inl.

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◆ GetGust_WaveLength()

su2double CConfig::GetGust_WaveLength ( void  )
inline

Value of the gust wavelength.

Definition at line 1725 of file config_structure.inl.

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◆ GetHarmonicBalance_Period()

su2double CConfig::GetHarmonicBalance_Period ( void  )
inline

Retrieves the period of oscillations to be used with Harmonic Balance.

Returns
: Period for Harmonic Balance.

Definition at line 298 of file config_structure.inl.

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◆ GetHB_Precondition()

bool CConfig::GetHB_Precondition ( void  )
inline

Get if harmonic balance source term is to be preconditioned.

Returns
yes or no to harmonic balance preconditioning

Definition at line 46 of file config_structure.inl.

◆ GetHeat_FileName()

string CConfig::GetHeat_FileName ( void  )
inline

Get the name of the file with the wave variables.

Returns
Name of the file with the wave variables.

Definition at line 1465 of file config_structure.inl.

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◆ GetHeat_Flux_Ref()

su2double CConfig::GetHeat_Flux_Ref ( void  )
inline

Get the reference value for the heat flux.

Returns
Reference value for the heat flux.

Definition at line 478 of file config_structure.inl.

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◆ GetHighlite_Area()

su2double CConfig::GetHighlite_Area ( void  )
inline

Get the value of the reference viscosity for non-dimensionalization.

Returns
Reference viscosity for non-dimensionalization.

Definition at line 528 of file config_structure.inl.

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◆ GetHistFile()

ofstream * CConfig::GetHistFile ( void  )
inline

Retrieve the ofstream of the history file for the current zone.

Definition at line 1963 of file config_structure.inl.

◆ GetHold_GridFixed()

bool CConfig::GetHold_GridFixed ( void  )
inline

Provides information about the the nodes that are going to be moved on a deformation volumetric grid deformation.

Returns
TRUE means that only the points on the FFD box will be moved.

Definition at line 1619 of file config_structure.inl.

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◆ GetHold_GridFixed_Coord()

su2double * CConfig::GetHold_GridFixed_Coord ( void  )
inline

Get the the coordinates where of the box where the grid is going to be deformed.

Returns
Coordinates where of the box where the grid is going to be deformed.

Definition at line 338 of file config_structure.inl.

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◆ GetHTP_Axis()

su2double CConfig::GetHTP_Axis ( unsigned short  val_index)
inline

Get the values of the CFL adapation.

Returns
Value of CFL adapation

Definition at line 40 of file config_structure.inl.

◆ GetiInst()

unsigned short CConfig::GetiInst ( void  )
inline

Get the current instance.

Returns
Current instance identifier.

Definition at line 1821 of file config_structure.inl.

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◆ GetInc_Density_Init()

su2double CConfig::GetInc_Density_Init ( void  )
inline

Get the value of the initial density for incompressible flows.

Returns
Initial density for incompressible flows.

Definition at line 472 of file config_structure.inl.

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◆ GetInc_Density_Ref()

su2double CConfig::GetInc_Density_Ref ( void  )
inline

Get the value of the reference density for custom incompressible non-dimensionalization.

Returns
Reference density for custom incompressible non-dimensionalization.

Definition at line 466 of file config_structure.inl.

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◆ GetInc_Inlet_UseNormal()

bool CConfig::GetInc_Inlet_UseNormal ( void  )
inline

Flag for whether the local boundary normal is used as the flow direction for an incompressible pressure inlet.

Returns
FALSE means the prescribed flow direction is used.

Definition at line 1174 of file config_structure.inl.

◆ GetInc_Temperature_Init()

su2double CConfig::GetInc_Temperature_Init ( void  )
inline

Get the value of the initial temperature for incompressible flows.

Returns
Initial temperature for incompressible flows.

Definition at line 476 of file config_structure.inl.

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◆ GetInc_Temperature_Ref()

su2double CConfig::GetInc_Temperature_Ref ( void  )
inline

Get the value of the reference temperature for custom incompressible non-dimensionalization.

Returns
Reference temperature for custom incompressible non-dimensionalization.

Definition at line 470 of file config_structure.inl.

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◆ GetInc_Velocity_Init()

su2double * CConfig::GetInc_Velocity_Init ( void  )
inline

Get the value of the initial velocity for incompressible flows.

Returns
Initial velocity for incompressible flows.

Definition at line 474 of file config_structure.inl.

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◆ GetInc_Velocity_Ref()

su2double CConfig::GetInc_Velocity_Ref ( void  )
inline

Get the value of the reference velocity for custom incompressible non-dimensionalization.

Returns
Reference velocity for custom incompressible non-dimensionalization.

Definition at line 468 of file config_structure.inl.

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◆ GetIncInlet_BC()

su2double CConfig::GetIncInlet_BC ( )

Get the inlet velocity or pressure imposed for incompressible flow.

Returns
inlet velocity or pressure

Definition at line 7893 of file config_structure.cpp.

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◆ GetIncLoad_Criteria()

su2double CConfig::GetIncLoad_Criteria ( unsigned short  val_var)
inline

Get the value of the criteria for applying incremental loading.

Returns
Value of the log10 of the residual.

Definition at line 1865 of file config_structure.inl.

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◆ GetInconsistent_Disc()

bool CConfig::GetInconsistent_Disc ( void  )
inline

Provides information about using an inconsistent (primal/dual) discrete adjoint formulation.

Returns
FALSE means that the adjoint use the same numerical methods than the primal problem.

Definition at line 1613 of file config_structure.inl.

◆ GetIncPressureOut_BC()

su2double CConfig::GetIncPressureOut_BC ( )

Get the outlet pressure imposed as BC for incompressible flow.

Returns
outlet pressure

Definition at line 7937 of file config_structure.cpp.

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◆ GetIncrementalLoad()

bool CConfig::GetIncrementalLoad ( void  )
inline

Check if we want to apply an incremental load to the nonlinear structural simulation.

Returns
TRUE means that the load is to be applied in increments.

Definition at line 1861 of file config_structure.inl.

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◆ GetIncTemperature_BC()

su2double CConfig::GetIncTemperature_BC ( )

Get the inlet temperature imposed as BC for incompressible flow.

Returns
inlet temperature

Definition at line 7918 of file config_structure.cpp.

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◆ GetInflow_Force()

su2double CConfig::GetInflow_Force ( string  val_marker)

Get the force balance at an engine inflow boundary.

Parameters
[in]val_marker- Name of the boundary.
Returns
The engine inflow force balance.

Definition at line 8142 of file config_structure.cpp.

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◆ GetInflow_Mach()

su2double CConfig::GetInflow_Mach ( string  val_marker)

Get the fan face Mach number at an engine inflow boundary.

Parameters
[in]val_marker- Name of the boundary.
Returns
The fan face Mach number.

Definition at line 8156 of file config_structure.cpp.

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◆ GetInflow_MassFlow()

su2double CConfig::GetInflow_MassFlow ( string  val_marker)

Get the mass flow rate at an engine inflow boundary.

Parameters
[in]val_marker- Name of the boundary.
Returns
The engine mass flow rate.

Definition at line 8100 of file config_structure.cpp.

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◆ GetInflow_Power()

su2double CConfig::GetInflow_Power ( string  val_marker)

Get the power at an engine inflow boundary.

Parameters
[in]val_marker- Name of the boundary.
Returns
The engine inflow power.

Definition at line 8149 of file config_structure.cpp.

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◆ GetInflow_Pressure()

su2double CConfig::GetInflow_Pressure ( string  val_marker)

Get the back pressure (static) at an engine inflow boundary.

Parameters
[in]val_marker- Name of the boundary.
Returns
The engine inflow pressure.

Definition at line 8093 of file config_structure.cpp.

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◆ GetInflow_RamDrag()

su2double CConfig::GetInflow_RamDrag ( string  val_marker)

Get the ram drag at an engine inflow boundary.

Parameters
[in]val_marker- Name of the boundary.
Returns
The engine inflow ram drag.

Definition at line 8135 of file config_structure.cpp.

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◆ GetInflow_ReverseMassFlow() [1/2]

su2double CConfig::GetInflow_ReverseMassFlow ( string  val_marker)

Get the percentage of reverse flow at an engine inflow boundary.

Parameters
[in]val_marker- Name of the boundary.
Returns
The percentage of reverse flow.

Definition at line 8107 of file config_structure.cpp.

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◆ GetInflow_ReverseMassFlow() [2/2]

su2double CConfig::GetInflow_ReverseMassFlow ( unsigned short  val_marker)
inline

Get the percentage of reverse flow at an engine inflow boundary.

Parameters
[in]val_index- Index corresponding to the engine inflow boundary.
Returns
The percentage of reverse flow.

Definition at line 68 of file config_structure.inl.

◆ GetInflow_Temperature()

su2double CConfig::GetInflow_Temperature ( string  val_marker)

Get the temperature (static) at an engine inflow boundary.

Parameters
[in]val_marker- Name of the boundary.
Returns
The engine inflow temperature.

Definition at line 8121 of file config_structure.cpp.

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◆ GetInflow_TotalPressure()

su2double CConfig::GetInflow_TotalPressure ( string  val_marker)

Get the total pressure at an engine inflow boundary.

Parameters
[in]val_marker- Name of the boundary.
Returns
The total pressure.

Definition at line 8114 of file config_structure.cpp.

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◆ GetInflow_TotalTemperature()

su2double CConfig::GetInflow_TotalTemperature ( string  val_marker)

Get the total temperature at an engine inflow boundary.

Parameters
[in]val_marker- Name of the boundary.
Returns
The engine inflow total temperature.

Definition at line 8128 of file config_structure.cpp.

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◆ GetInitial_BCThrust()

su2double CConfig::GetInitial_BCThrust ( void  )
inline

Get the value of the non-dimensionalized actuator disk turbulence intensity.

Returns
Non-dimensionalized actuator disk intensity.

Definition at line 566 of file config_structure.inl.

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◆ GetInitial_Gas_Composition()

su2double CConfig::GetInitial_Gas_Composition ( unsigned short  iSpecies)

Provides the molar mass of each species present in multi species fluid.

Returns
: Molar mass of the specified gas consituent [kg/kmol]

◆ GetInlet_FileName()

string CConfig::GetInlet_FileName ( void  )
inline

Get name of the input file for the specified inlet profile.

Returns
Name of the input file for the specified inlet profile.

Definition at line 1168 of file config_structure.inl.

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◆ GetInlet_FlowDir()

su2double * CConfig::GetInlet_FlowDir ( string  val_index)

Get the flow direction unit vector at an inlet boundary.

Parameters
[in]val_index- Index corresponding to the inlet boundary.
Returns
The flow direction vector.

Definition at line 7663 of file config_structure.cpp.

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◆ GetInlet_Pressure()

su2double CConfig::GetInlet_Pressure ( string  val_index)

Get the pressure at a supersonic inlet boundary.

Parameters
[in]val_index- Index corresponding to the inlet boundary.
Returns
The inlet pressure.

Definition at line 7677 of file config_structure.cpp.

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◆ GetInlet_Profile_From_File()

bool CConfig::GetInlet_Profile_From_File ( void  )
inline

Check if the inlet profile(s) are specified in an input file.

Returns
True if an input file is to be used for the inlet profile(s)

Definition at line 1166 of file config_structure.inl.

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◆ GetInlet_Profile_Matching_Tolerance()

su2double CConfig::GetInlet_Profile_Matching_Tolerance ( void  )
inline

Get the tolerance used for matching two points on a specified inlet.

Returns
Tolerance used for matching a point to a specified inlet

Definition at line 1170 of file config_structure.inl.

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◆ GetInlet_Ptotal()

su2double CConfig::GetInlet_Ptotal ( string  val_index)

Get the total pressure at an inlet boundary.

Parameters
[in]val_index- Index corresponding to the inlet boundary.
Returns
The total pressure.

Definition at line 7649 of file config_structure.cpp.

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◆ GetInlet_Temperature()

su2double CConfig::GetInlet_Temperature ( string  val_index)

Get the temperature at a supersonic inlet boundary.

Parameters
[in]val_index- Index corresponding to the inlet boundary.
Returns
The inlet density.

Definition at line 7670 of file config_structure.cpp.

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◆ GetInlet_Ttotal()

su2double CConfig::GetInlet_Ttotal ( string  val_index)

Get the total temperature at an inlet boundary.

Parameters
[in]val_index- Index corresponding to the inlet boundary.
Returns
The total temperature.

Definition at line 7642 of file config_structure.cpp.

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◆ GetInlet_Velocity()

su2double * CConfig::GetInlet_Velocity ( string  val_index)

Get the velocity vector at a supersonic inlet boundary.

Parameters
[in]val_index- Index corresponding to the inlet boundary.
Returns
The inlet velocity vector.

Definition at line 7684 of file config_structure.cpp.

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◆ GetIntegrated_HeatFlux()

bool CConfig::GetIntegrated_HeatFlux ( void  )
inline

Check if values passed to the BC_HeatFlux-Routine are already integrated.

Returns
YES if the passed values is the integrated heat flux over the marker's surface.

Definition at line 1933 of file config_structure.inl.

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◆ GetIntermittency_FreeStream()

su2double CConfig::GetIntermittency_FreeStream ( void  )
inline

Get the value of the non-dimensionalized freestream intermittency.

Returns
Non-dimensionalized freestream intermittency.

Definition at line 570 of file config_structure.inl.

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◆ GetIntIter()

unsigned long CConfig::GetIntIter ( void  )
inline

Get the current internal iteration number.

Returns
Current internal iteration.

Definition at line 314 of file config_structure.inl.

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◆ GetInvDesign_Cp()

bool CConfig::GetInvDesign_Cp ( void  )
inline

Information about computing and plotting the equivalent area distribution.

Returns
TRUE or FALSE depending if we are computing the equivalent area.

Definition at line 1296 of file config_structure.inl.

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◆ GetInvDesign_HeatFlux()

bool CConfig::GetInvDesign_HeatFlux ( void  )
inline

Information about computing and plotting the equivalent area distribution.

Returns
TRUE or FALSE depending if we are computing the equivalent area.

Definition at line 1298 of file config_structure.inl.

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◆ GetIonization()

bool CConfig::GetIonization ( void  )

Indicates whether electron gas is present in the gas mixture.

◆ GetIsothermal_Temperature()

su2double CConfig::GetIsothermal_Temperature ( string  val_index)

Get the wall temperature (static) at an isothermal boundary.

Parameters
[in]val_index- Index corresponding to the isothermal boundary.
Returns
The wall temperature.

Definition at line 7960 of file config_structure.cpp.

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◆ GetIsothermalWall()

bool CConfig::GetIsothermalWall ( void  )

Get information about the isothermal wall condition.

Returns
TRUE if it is a isothermal wall condition; otherwise FALSE.

◆ GetIter_Avg_Objective()

unsigned long CConfig::GetIter_Avg_Objective ( void  )
inline

Number of iterations to average (reverse time integration).

Returns
Starting direct iteration number for the unsteady adjoint.

Definition at line 326 of file config_structure.inl.

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◆ GetIter_dCL_dAlpha()

unsigned long CConfig::GetIter_dCL_dAlpha ( void  )
inline

Number of iterations to evaluate dCL_dAlpha.

Returns
Number of iterations.

Definition at line 1769 of file config_structure.inl.

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◆ GetIter_Fixed_CL()

unsigned long CConfig::GetIter_Fixed_CL ( void  )
inline

Get the value of iterations to re-evaluate the angle of attack.

Returns
Number of iterations.

Definition at line 1765 of file config_structure.inl.

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◆ GetIter_Fixed_NetThrust()

unsigned long CConfig::GetIter_Fixed_NetThrust ( void  )
inline

Get the value of iterations to re-evaluate the angle of attack.

Returns
Number of iterations.

Definition at line 1763 of file config_structure.inl.

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◆ GetiZone()

unsigned short CConfig::GetiZone ( void  )
inline

Provides the number of varaibles.

Returns
Number of variables.

Definition at line 280 of file config_structure.inl.

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◆ GetJacobian_Spatial_Discretization_Only()

bool CConfig::GetJacobian_Spatial_Discretization_Only ( void  )
inline

Function to make available whether or not only the exact Jacobian of the spatial discretization must be computed.

Returns
The boolean whether or not the Jacobian must be computed.

Definition at line 1929 of file config_structure.inl.

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◆ GetKappa_1st_AdjFlow()

su2double CConfig::GetKappa_1st_AdjFlow ( void  )
inline

Value of the calibrated constant for the low order method (center scheme).

Returns
Calibrated constant for the low order center method for the adjoint flow equations.

Definition at line 1140 of file config_structure.inl.

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◆ GetKappa_1st_Flow()

su2double CConfig::GetKappa_1st_Flow ( void  )
inline

Value of the calibrated constant for the Lax method (center scheme).

Note
This constant is used in coarse levels and with first order methods.
Returns
Calibrated constant for the Lax method.

Definition at line 1122 of file config_structure.inl.

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◆ GetKappa_2nd_AdjFlow()

su2double CConfig::GetKappa_2nd_AdjFlow ( void  )
inline

Value of the calibrated constant for the high order method (center scheme).

Returns
Calibrated constant for the high order center method for the adjoint flow equations.

Definition at line 1142 of file config_structure.inl.

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◆ GetKappa_2nd_Flow()

su2double CConfig::GetKappa_2nd_Flow ( void  )
inline

Value of the calibrated constant for the JST method (center scheme).

Returns
Calibrated constant for the JST method for the flow equations.

Definition at line 1124 of file config_structure.inl.

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◆ GetKappa_2nd_Heat()

su2double CConfig::GetKappa_2nd_Heat ( void  )
inline

Value of the calibrated constant for the JST method (center scheme).

Returns
Calibrated constant for the JST-like method for the heat equations.

Definition at line 1128 of file config_structure.inl.

◆ GetKappa_4th_AdjFlow()

su2double CConfig::GetKappa_4th_AdjFlow ( void  )
inline

Value of the calibrated constant for the high order method (center scheme).

Returns
Calibrated constant for the high order center method for the adjoint flow equations.

Definition at line 1144 of file config_structure.inl.

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◆ GetKappa_4th_Flow()

su2double CConfig::GetKappa_4th_Flow ( void  )
inline

Value of the calibrated constant for the JST method (center scheme).

Returns
Calibrated constant for the JST method for the flow equations.

Definition at line 1126 of file config_structure.inl.

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◆ GetKappa_4th_Heat()

su2double CConfig::GetKappa_4th_Heat ( void  )
inline

Value of the calibrated constant for the JST-like method (center scheme).

Returns
Calibrated constant for the JST-like method for the heat equation.

Definition at line 1130 of file config_structure.inl.

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◆ GetKind_ActDisk()

unsigned short CConfig::GetKind_ActDisk ( void  )
inline

Get the kind of inlet boundary condition treatment (total conditions or mass flow).

Returns
Kind of inlet boundary condition.

Definition at line 1178 of file config_structure.inl.

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◆ GetKind_Adaptation()

unsigned short CConfig::GetKind_Adaptation ( void  )
inline

Get the kind of adaptation technique.

Returns
Kind of adaptation technique.

Definition at line 1058 of file config_structure.inl.

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◆ GetKind_ADER_Predictor()

unsigned short CConfig::GetKind_ADER_Predictor ( void  )
inline

Get the kind of scheme (aliased or non-aliased) to be used in the predictor step of ADER-DG.

Returns
Kind of scheme used in the predictor step of ADER-DG.

Definition at line 1084 of file config_structure.inl.

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◆ GetKind_AdjTurb_Linear_Prec()

unsigned short CConfig::GetKind_AdjTurb_Linear_Prec ( void  )
inline

Get the kind of preconditioner for the implicit solver.

Returns
Numerical preconditioner for implicit formulation (solving the linear system).

Definition at line 1016 of file config_structure.inl.

◆ GetKind_AdjTurb_Linear_Solver()

unsigned short CConfig::GetKind_AdjTurb_Linear_Solver ( void  )
inline

Get the kind of solver for the implicit solver.

Returns
Numerical solver for implicit formulation (solving the linear system).

Definition at line 1014 of file config_structure.inl.

◆ GetKind_Average()

unsigned short CConfig::GetKind_Average ( void  )
inline

Get the kind of marker analyze marker (area-averaged, mass flux averaged, etc).

Returns
Kind of average.

Definition at line 1793 of file config_structure.inl.

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◆ GetKind_AverageProcess()

unsigned short CConfig::GetKind_AverageProcess ( void  )
inline

Get the kind of mixing process for averaging quantities at the boundaries.

Returns
Kind of mixing process.

Definition at line 1182 of file config_structure.inl.

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◆ GetKind_Centered()

unsigned short CConfig::GetKind_Centered ( void  )
inline

Get kind of center scheme for the convective terms.

Note
This is the information that the code will use, the method will change in runtime depending of the specific equation (direct, adjoint, linearized) that is being solved.
Returns
Kind of center scheme for the convective terms.

Definition at line 1066 of file config_structure.inl.

◆ GetKind_Centered_AdjFlow()

unsigned short CConfig::GetKind_Centered_AdjFlow ( void  )
inline

Get the kind of center convective numerical scheme for the adjoint flow equations.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of center convective numerical scheme for the adjoint flow equations.

Definition at line 1136 of file config_structure.inl.

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◆ GetKind_Centered_AdjTurb()

unsigned short CConfig::GetKind_Centered_AdjTurb ( void  )
inline

Get the kind of center convective numerical scheme for the adjoint turbulence equations.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of center convective numerical scheme for the adjoint turbulence equations.

Definition at line 1158 of file config_structure.inl.

◆ GetKind_Centered_Flow()

unsigned short CConfig::GetKind_Centered_Flow ( void  )
inline

Get the kind of center convective numerical scheme for the flow equations.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of center convective numerical scheme for the flow equations.

Definition at line 1102 of file config_structure.inl.

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◆ GetKind_Centered_Template()

unsigned short CConfig::GetKind_Centered_Template ( void  )

Get the kind of center convective numerical scheme for the plasma equations.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of center convective numerical scheme for the flow equations.

◆ GetKind_Centered_Turb()

unsigned short CConfig::GetKind_Centered_Turb ( void  )
inline

Get the kind of center convective numerical scheme for the turbulence equations.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of center convective numerical scheme for the turbulence equations.

Definition at line 1150 of file config_structure.inl.

◆ GetKind_ConductivityModel()

unsigned short CConfig::GetKind_ConductivityModel ( void  )
inline

Get the value of the thermal conductivity model.

Returns
Connectivity model.

Definition at line 874 of file config_structure.inl.

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◆ GetKind_ConvNumScheme()

unsigned short CConfig::GetKind_ConvNumScheme ( void  )
inline

Get the kind of convective numerical scheme.

Note
This is the information that the code will use, the method will change in runtime depending of the specific equation (direct, adjoint, linearized) that is being solved.
Returns
Kind of the convective scheme.

Definition at line 1064 of file config_structure.inl.

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◆ GetKind_ConvNumScheme_AdjFlow()

unsigned short CConfig::GetKind_ConvNumScheme_AdjFlow ( void  )
inline

Get the kind of convective numerical scheme for the adjoint flow equations (centered or upwind).

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of convective numerical scheme for the adjoint flow equations.

Definition at line 1134 of file config_structure.inl.

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◆ GetKind_ConvNumScheme_AdjTurb()

unsigned short CConfig::GetKind_ConvNumScheme_AdjTurb ( void  )
inline

Get the kind of convective numerical scheme for the adjoint turbulence equations (centered or upwind).

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of convective numerical scheme for the adjoint turbulence equations.

Definition at line 1156 of file config_structure.inl.

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◆ GetKind_ConvNumScheme_FEM_Flow()

unsigned short CConfig::GetKind_ConvNumScheme_FEM_Flow ( void  )
inline

Get the kind of convective numerical scheme for the flow equations (finite element).

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of convective numerical scheme for the flow equations.

Definition at line 1098 of file config_structure.inl.

◆ GetKind_ConvNumScheme_Flow()

unsigned short CConfig::GetKind_ConvNumScheme_Flow ( void  )
inline

Get the kind of convective numerical scheme for the flow equations (centered or upwind).

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of convective numerical scheme for the flow equations.

Definition at line 1096 of file config_structure.inl.

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◆ GetKind_ConvNumScheme_Heat()

unsigned short CConfig::GetKind_ConvNumScheme_Heat ( void  )
inline

Get the kind of convective numerical scheme for the heat equation.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of convective numerical scheme for the heat equation.

Definition at line 1162 of file config_structure.inl.

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◆ GetKind_ConvNumScheme_Template()

unsigned short CConfig::GetKind_ConvNumScheme_Template ( void  )
inline

Get the kind of convective numerical scheme for the template equations (centered or upwind).

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of convective numerical scheme for the flow equations.

Definition at line 1100 of file config_structure.inl.

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◆ GetKind_ConvNumScheme_Turb()

unsigned short CConfig::GetKind_ConvNumScheme_Turb ( void  )
inline

Get the kind of convective numerical scheme for the turbulence equations (upwind).

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of convective numerical scheme for the turbulence equations.

Definition at line 1148 of file config_structure.inl.

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◆ GetKind_Data_Giles()

unsigned short CConfig::GetKind_Data_Giles ( string  val_marker)

Get Kind Data for the Giles BC.

Parameters
[in]val_marker- Index corresponding to the Giles BC.
Returns
Kind data

Definition at line 7776 of file config_structure.cpp.

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◆ GetKind_Data_Riemann()

unsigned short CConfig::GetKind_Data_Riemann ( string  val_marker)

Get Kind Data of Riemann boundary.

Parameters
[in]val_marker- Index corresponding to the Riemann boundary.
Returns
Kind data

Definition at line 7726 of file config_structure.cpp.

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◆ GetKind_Deform_Linear_Solver()

unsigned short CConfig::GetKind_Deform_Linear_Solver ( void  )
inline

Get the kind of solver for the implicit solver.

Returns
Numerical solver for implicit formulation (solving the linear system).

Definition at line 982 of file config_structure.inl.

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◆ GetKind_Deform_Linear_Solver_Prec()

unsigned short CConfig::GetKind_Deform_Linear_Solver_Prec ( void  )
inline

Get the kind of preconditioner for the implicit solver.

Returns
Numerical preconditioner for implicit formulation (solving the linear system).

Definition at line 1022 of file config_structure.inl.

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◆ GetKind_DensityModel()

unsigned short CConfig::GetKind_DensityModel ( void  )
inline

Option to define the density model for incompressible flows.

Returns
Density model option

Definition at line 860 of file config_structure.inl.

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◆ GetKind_DiscAdj_Linear_Prec()

unsigned short CConfig::GetKind_DiscAdj_Linear_Prec ( void  )
inline

Get the kind of preconditioner for the implicit solver.

Returns
Numerical preconditioner for implicit formulation (solving the linear system).

Definition at line 1020 of file config_structure.inl.

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◆ GetKind_DiscAdj_Linear_Solver()

unsigned short CConfig::GetKind_DiscAdj_Linear_Solver ( void  )
inline

Get the kind of solver for the implicit solver.

Returns
Numerical solver for implicit formulation (solving the linear system).

Definition at line 1018 of file config_structure.inl.

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◆ GetKind_Engine_Inflow()

unsigned short CConfig::GetKind_Engine_Inflow ( void  )
inline

Get the kind of inlet boundary condition treatment (total conditions or mass flow).

Returns
Kind of inlet boundary condition.

Definition at line 1176 of file config_structure.inl.

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◆ GetKind_FEM_DG_Shock()

unsigned short CConfig::GetKind_FEM_DG_Shock ( void  )
inline

Get the kind of shock capturing method in FEM DG solver.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of shock capturing method in FEM DG solver.

Definition at line 1118 of file config_structure.inl.

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◆ GetKind_FEM_Flow()

unsigned short CConfig::GetKind_FEM_Flow ( void  )
inline

Get the kind of finite element convective numerical scheme for the flow equations.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of finite element convective numerical scheme for the flow equations.

Definition at line 1116 of file config_structure.inl.

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◆ GetKind_FluidModel()

unsigned short CConfig::GetKind_FluidModel ( void  )
inline

Fluid model that we are using.

Returns
Fluid model that we are using.

Definition at line 856 of file config_structure.inl.

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◆ GetKind_FreeStreamOption()

unsigned short CConfig::GetKind_FreeStreamOption ( void  )
inline

free stream option to initialize the solution

Returns
free stream option

Definition at line 858 of file config_structure.inl.

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◆ GetKind_GasModel()

unsigned short CConfig::GetKind_GasModel ( void  )
inline

Gas model that we are using.

Returns
Gas model that we are using.

Definition at line 854 of file config_structure.inl.

◆ GetKind_Gradient_Method()

unsigned short CConfig::GetKind_Gradient_Method ( void  )
inline

Get the kind of method for computation of spatial gradients.

Returns
Numerical method for computation of spatial gradients.

Definition at line 978 of file config_structure.inl.

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◆ GetKind_GridMovement()

unsigned short CConfig::GetKind_GridMovement ( unsigned short  val_iZone)
inline

Get the type of dynamic mesh motion.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Type of dynamic mesh motion.

Definition at line 906 of file config_structure.inl.

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◆ GetKind_HybridRANSLES()

unsigned short CConfig::GetKind_HybridRANSLES ( void  )
inline

Get the Kind of Hybrid RANS/LES.

Returns
Value of Hybrid RANS/LES method.

Definition at line 1953 of file config_structure.inl.

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◆ GetKind_Inc_Inlet()

unsigned short CConfig::GetKind_Inc_Inlet ( string  val_marker)

Get the type of incompressible inlet from the list.

Returns
Kind of the incompressible inlet.

Definition at line 7635 of file config_structure.cpp.

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◆ GetKind_InitOption()

unsigned short CConfig::GetKind_InitOption ( void  )
inline

free stream option to initialize the solution

Returns
free stream option

Definition at line 864 of file config_structure.inl.

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◆ GetKind_Inlet()

unsigned short CConfig::GetKind_Inlet ( void  )
inline

Get the kind of inlet boundary condition treatment (total conditions or mass flow).

Returns
Kind of inlet boundary condition.

Definition at line 1164 of file config_structure.inl.

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◆ GetKind_Linear_Solver()

unsigned short CConfig::GetKind_Linear_Solver ( void  )
inline

Get the kind of solver for the implicit solver.

Returns
Numerical solver for implicit formulation (solving the linear system).

Definition at line 980 of file config_structure.inl.

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◆ GetKind_Linear_Solver_Prec()

unsigned short CConfig::GetKind_Linear_Solver_Prec ( void  )
inline

Get the kind of preconditioner for the implicit solver.

Returns
Numerical preconditioner for implicit formulation (solving the linear system).

Definition at line 986 of file config_structure.inl.

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◆ GetKind_Matrix_Coloring()

unsigned short CConfig::GetKind_Matrix_Coloring ( void  )
inline

Get the kind of matrix coloring used for the sparse Jacobian computation.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of matrix coloring used.

Definition at line 1120 of file config_structure.inl.

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◆ GetKind_MixingPlaneInterface()

unsigned short CConfig::GetKind_MixingPlaneInterface ( void  )
inline

Get the kind of mixing process for averaging quantities at the boundaries.

Returns
Kind of mixing process.

Definition at line 1210 of file config_structure.inl.

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◆ GetKind_ObjFunc() [1/2]

unsigned short CConfig::GetKind_ObjFunc ( unsigned short  val_obj)
inline

Get the kind of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc.

Author
H. Kline
Note
The objective function will determine the boundary condition of the adjoint problem.
Returns
Kind of objective function.

Definition at line 1274 of file config_structure.inl.

◆ GetKind_ObjFunc() [2/2]

unsigned short CConfig::GetKind_ObjFunc ( void  )
inline

Get the kind of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc.

Note
The objective function will determine the boundary condition of the adjoint problem.
Returns
Kind of objective function.

Definition at line 1272 of file config_structure.inl.

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◆ GetKind_PerformanceAverageProcess()

unsigned short CConfig::GetKind_PerformanceAverageProcess ( void  )
inline

Get the kind of mixing process for averaging quantities at the boundaries.

Returns
Kind of mixing process.

Definition at line 1184 of file config_structure.inl.

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◆ GetKind_Regime()

unsigned short CConfig::GetKind_Regime ( void  )
inline

Governing equations of the flow (it can be different from the run time equation).

Parameters
[in]val_zone- Zone where the soler is applied.
Returns
Governing equation that we are solving.

Definition at line 850 of file config_structure.inl.

◆ GetKind_RoeLowDiss()

unsigned short CConfig::GetKind_RoeLowDiss ( void  )
inline

Get the Kind of Roe Low Dissipation Scheme for Unsteady flows.

Returns
Value of Low dissipation approach.

Definition at line 1955 of file config_structure.inl.

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◆ GetKind_SensSmooth()

unsigned short CConfig::GetKind_SensSmooth ( void  )
inline

Get the kind of sensitivity smoothing technique.

Returns
Kind of sensitivity smoothing technique.

Definition at line 1282 of file config_structure.inl.

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◆ GetKind_SGS_Model()

unsigned short CConfig::GetKind_SGS_Model ( void  )
inline

Get the kind of the subgrid scale model.

Returns
Kind of the subgrid scale model.

Definition at line 1605 of file config_structure.inl.

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◆ GetKind_SlopeLimit()

unsigned short CConfig::GetKind_SlopeLimit ( void  )
inline

Get the method for limiting the spatial gradients.

Returns
Method for limiting the spatial gradients.

Definition at line 1104 of file config_structure.inl.

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◆ GetKind_SlopeLimit_AdjFlow()

unsigned short CConfig::GetKind_SlopeLimit_AdjFlow ( void  )
inline

Get the method for limiting the spatial gradients.

Returns
Method for limiting the spatial gradients solving the adjoint flow equation.

Definition at line 1112 of file config_structure.inl.

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◆ GetKind_SlopeLimit_AdjTurb()

unsigned short CConfig::GetKind_SlopeLimit_AdjTurb ( void  )
inline

Get the method for limiting the spatial gradients.

Returns
Method for limiting the spatial gradients solving the adjoint turbulent equation.

Definition at line 1110 of file config_structure.inl.

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◆ GetKind_SlopeLimit_Flow()

unsigned short CConfig::GetKind_SlopeLimit_Flow ( void  )
inline

Get the method for limiting the spatial gradients.

Returns
Method for limiting the spatial gradients solving the flow equations.

Definition at line 1106 of file config_structure.inl.

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◆ GetKind_SlopeLimit_Turb()

unsigned short CConfig::GetKind_SlopeLimit_Turb ( void  )
inline

Get the method for limiting the spatial gradients.

Returns
Method for limiting the spatial gradients solving the turbulent equation.

Definition at line 1108 of file config_structure.inl.

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◆ GetKind_Solver()

unsigned short CConfig::GetKind_Solver ( void  )
inline

Governing equations of the flow (it can be different from the run time equation).

Parameters
[in]val_zone- Zone where the soler is applied.
Returns
Governing equation that we are solving.

Definition at line 846 of file config_structure.inl.

◆ GetKind_SpaceIteScheme_FEA()

unsigned short CConfig::GetKind_SpaceIteScheme_FEA ( void  )
inline

Get the kind of integration scheme (explicit or implicit) for the flow equations.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of integration scheme for the plasma equations.

Definition at line 1092 of file config_structure.inl.

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◆ GetKind_SpanWise()

unsigned short CConfig::GetKind_SpanWise ( void  )
inline

Get the kind of turbomachinery architecture.

Returns
Kind of turbomachinery architecture.

Definition at line 1214 of file config_structure.inl.

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◆ GetKind_SU2()

unsigned short CConfig::GetKind_SU2 ( void  )
inline

Get the kind of SU2 software component.

Returns
Kind of the SU2 software component.

Definition at line 282 of file config_structure.inl.

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◆ GetKind_TimeIntScheme()

unsigned short CConfig::GetKind_TimeIntScheme ( void  )
inline

Get the kind of time integration method.

Note
This is the information that the code will use, the method will change in runtime depending of the specific equation (direct, adjoint, linearized) that is being solved.
Returns
Kind of time integration method.

Definition at line 1062 of file config_structure.inl.

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◆ GetKind_TimeIntScheme_AdjFlow()

unsigned short CConfig::GetKind_TimeIntScheme_AdjFlow ( void  )
inline

Get the kind of integration scheme (explicit or implicit) for the adjoint flow equations.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of integration scheme for the adjoint flow equations.

Definition at line 1132 of file config_structure.inl.

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◆ GetKind_TimeIntScheme_AdjTurb()

unsigned short CConfig::GetKind_TimeIntScheme_AdjTurb ( void  )
inline

Get the kind of integration scheme (explicit or implicit) for the adjoint turbulence equations.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of integration scheme for the adjoint turbulence equations.

Definition at line 1154 of file config_structure.inl.

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◆ GetKind_TimeIntScheme_FEA()

unsigned short CConfig::GetKind_TimeIntScheme_FEA ( void  )
inline

Get the kind of integration scheme (explicit or implicit) for the flow equations.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of integration scheme for the plasma equations.

Definition at line 1090 of file config_structure.inl.

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◆ GetKind_TimeIntScheme_Flow()

unsigned short CConfig::GetKind_TimeIntScheme_Flow ( void  )
inline

Get the kind of integration scheme (explicit or implicit) for the flow equations.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of integration scheme for the flow equations.

Definition at line 1082 of file config_structure.inl.

◆ GetKind_TimeIntScheme_Heat()

unsigned short CConfig::GetKind_TimeIntScheme_Heat ( void  )
inline

Get the kind of integration scheme (explicit or implicit) for the flow equations.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of integration scheme for the plasma equations.

Definition at line 1086 of file config_structure.inl.

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◆ GetKind_TimeIntScheme_Template()

unsigned short CConfig::GetKind_TimeIntScheme_Template ( void  )

Get the kind of integration scheme (explicit or implicit) for the template equations.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of integration scheme for the plasma equations.

◆ GetKind_TimeIntScheme_Turb()

unsigned short CConfig::GetKind_TimeIntScheme_Turb ( void  )
inline

Get the kind of integration scheme (implicit) for the turbulence equations.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of integration scheme for the turbulence equations.

Definition at line 1146 of file config_structure.inl.

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◆ GetKind_TimeStep_Heat()

unsigned short CConfig::GetKind_TimeStep_Heat ( void  )
inline

Get the kind of time stepping for the heat equation.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of time stepping for the heat equation.

Definition at line 1088 of file config_structure.inl.

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◆ GetKind_Trans_Model()

unsigned short CConfig::GetKind_Trans_Model ( void  )
inline

Get the kind of the transition model.

Returns
Kind of the transion model.

Definition at line 1603 of file config_structure.inl.

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◆ GetKind_TransferMethod()

unsigned short CConfig::GetKind_TransferMethod ( void  )
inline

Get the kind of transfer method we want to use for multiphysics problems.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of transfer method for multiphysics problems

Definition at line 1094 of file config_structure.inl.

◆ GetKind_Turb_Model()

unsigned short CConfig::GetKind_Turb_Model ( void  )
inline

Get the kind of the turbulence model.

Returns
Kind of the turbulence model.

Definition at line 1601 of file config_structure.inl.

◆ GetKind_TurboMachinery()

unsigned short CConfig::GetKind_TurboMachinery ( unsigned short  val_iZone)
inline

Get the kind of turbomachinery architecture.

Returns
Kind of turbomachinery architecture.

Definition at line 1212 of file config_structure.inl.

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◆ GetKind_TurboPerf()

unsigned short CConfig::GetKind_TurboPerf ( unsigned short  index)

get marker kind for Turbomachinery performance calculation.

Returns
kind index.

◆ GetKind_Upwind()

unsigned short CConfig::GetKind_Upwind ( void  )
inline

Get kind of upwind scheme for the convective terms.

Note
This is the information that the code will use, the method will change in runtime depending of the specific equation (direct, adjoint, linearized) that is being solved.
Returns
Kind of upwind scheme for the convective terms.

Definition at line 1068 of file config_structure.inl.

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◆ GetKind_Upwind_AdjFlow()

unsigned short CConfig::GetKind_Upwind_AdjFlow ( void  )
inline

Get the kind of upwind convective numerical scheme for the adjoint flow equations.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of upwind convective numerical scheme for the adjoint flow equations.

Definition at line 1138 of file config_structure.inl.

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◆ GetKind_Upwind_AdjTurb()

unsigned short CConfig::GetKind_Upwind_AdjTurb ( void  )
inline

Get the kind of upwind convective numerical scheme for the adjoint turbulence equations.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of upwind convective numerical scheme for the adjoint turbulence equations.

Definition at line 1160 of file config_structure.inl.

◆ GetKind_Upwind_Flow()

unsigned short CConfig::GetKind_Upwind_Flow ( void  )
inline

Get the kind of upwind convective numerical scheme for the flow equations.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of upwind convective numerical scheme for the flow equations.

Definition at line 1114 of file config_structure.inl.

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◆ GetKind_Upwind_Turb()

unsigned short CConfig::GetKind_Upwind_Turb ( void  )
inline

Get the kind of upwind convective numerical scheme for the turbulence equations.

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of upwind convective numerical scheme for the turbulence equations.

Definition at line 1152 of file config_structure.inl.

◆ GetKind_ViscosityModel()

unsigned short CConfig::GetKind_ViscosityModel ( void  )
inline

Get the value of the viscosity model.

Returns
Viscosity model.

Definition at line 872 of file config_structure.inl.

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◆ GetKindInterpolation()

unsigned short CConfig::GetKindInterpolation ( void  )
inline

Get the interpolation method used for matching between zones.

Definition at line 1875 of file config_structure.inl.

◆ GetKindRadialBasisFunction()

unsigned short CConfig::GetKindRadialBasisFunction ( void  )
inline

Get the basis function to use for radial basis function interpolation for FSI.

Definition at line 1877 of file config_structure.inl.

◆ GetKnowles_B()

su2double CConfig::GetKnowles_B ( void  )
inline

Get the value of the B constant in the Knowles material model.

Returns
Value of the B constant in the Knowles material model.

Definition at line 372 of file config_structure.inl.

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◆ GetKnowles_N()

su2double CConfig::GetKnowles_N ( void  )
inline

Get the value of the N constant in the Knowles material model.

Returns
Value of the N constant in the Knowles material model.

Definition at line 374 of file config_structure.inl.

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◆ GetKt_Constant()

su2double CConfig::GetKt_Constant ( void  )
inline

Get the value of the thermal conductivity.

Returns
Thermal conductivity.

Definition at line 880 of file config_structure.inl.

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◆ GetKt_ConstantND()

su2double CConfig::GetKt_ConstantND ( void  )
inline

Get the value of the non-dimensional thermal conductivity.

Returns
Non-dimensional thermal conductivity.

Definition at line 882 of file config_structure.inl.

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◆ GetLength_Ref()

su2double CConfig::GetLength_Ref ( void  )
inline

Get the value of the reference length for non-dimensionalization. This value should always be 1 internally, and is not user-specified.

Returns
Reference length for non-dimensionalization.

Definition at line 510 of file config_structure.inl.

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◆ GetLength_Reynolds()

su2double CConfig::GetLength_Reynolds ( void  )
inline

Get the value of the Reynolds length.

Returns
Reynolds length.

Definition at line 578 of file config_structure.inl.

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◆ GetLimiterIter()

unsigned long CConfig::GetLimiterIter ( void  )
inline

Freeze the value of the limiter after a number of iterations.

Returns
Number of iterations.

Definition at line 607 of file config_structure.inl.

◆ GetLinear_Solver_Error()

su2double CConfig::GetLinear_Solver_Error ( void  )
inline

Get min error of the linear solver for the implicit formulation.

Returns
Min error of the linear solver for the implicit formulation.

Definition at line 990 of file config_structure.inl.

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◆ GetLinear_Solver_ILU_n()

unsigned short CConfig::GetLinear_Solver_ILU_n ( void  )
inline

Get the ILU fill-in level for the linear solver.

Returns
Fill in level of the ILU preconditioner for the linear solver.

Definition at line 998 of file config_structure.inl.

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◆ GetLinear_Solver_Iter()

unsigned long CConfig::GetLinear_Solver_Iter ( void  )
inline

Get max number of iterations of the linear solver for the implicit formulation.

Returns
Max number of iterations of the linear solver for the implicit formulation.

Definition at line 994 of file config_structure.inl.

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◆ GetLinear_Solver_Restart_Frequency()

unsigned long CConfig::GetLinear_Solver_Restart_Frequency ( void  )
inline

Get restart frequency of the linear solver for the implicit formulation.

Returns
Restart frequency of the linear solver for the implicit formulation.

Definition at line 1000 of file config_structure.inl.

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◆ GetLoad_Dir()

su2double * CConfig::GetLoad_Dir ( string  val_index)

Get the force direction at a loaded boundary in cartesian coordinates.

Parameters
[in]val_index- Index corresponding to the load boundary.
Returns
The load direction.

Definition at line 8380 of file config_structure.cpp.

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◆ GetLoad_Dir_Multiplier()

su2double CConfig::GetLoad_Dir_Multiplier ( string  val_index)

Get the force multiplier at a load boundary in cartesian coordinates.

Parameters
[in]val_index- Index corresponding to the load boundary.
Returns
The load multiplier.

Definition at line 8359 of file config_structure.cpp.

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◆ GetLoad_Dir_Value()

su2double CConfig::GetLoad_Dir_Value ( string  val_index)

Get the force value at a load boundary defined in cartesian coordinates.

Parameters
[in]val_index- Index corresponding to the load boundary.
Returns
The load value.

Definition at line 8352 of file config_structure.cpp.

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◆ GetLoad_Sine()

su2double * CConfig::GetLoad_Sine ( void  )
inline

Get the sine load properties.

Parameters
[in]val_index- Index corresponding to the load boundary.
Returns
The pointer to the sine load values.

Definition at line 1853 of file config_structure.inl.

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◆ GetLoad_Sine_Amplitude()

su2double CConfig::GetLoad_Sine_Amplitude ( string  val_index)

Get the amplitude of the sine-wave at a load boundary defined in cartesian coordinates.

Parameters
[in]val_index- Index corresponding to the load boundary.
Returns
The load value.

Definition at line 8394 of file config_structure.cpp.

◆ GetLoad_Sine_Dir()

su2double * CConfig::GetLoad_Sine_Dir ( string  val_index)

Get the force direction at a sine-wave loaded boundary in cartesian coordinates.

Parameters
[in]val_index- Index corresponding to the load boundary.
Returns
The load direction.

Definition at line 8408 of file config_structure.cpp.

◆ GetLoad_Sine_Frequency()

su2double CConfig::GetLoad_Sine_Frequency ( string  val_index)

Get the frequency of the sine-wave at a load boundary in cartesian coordinates.

Parameters
[in]val_index- Index corresponding to the load boundary.
Returns
The load frequency.

Definition at line 8401 of file config_structure.cpp.

◆ GetLoad_Value()

su2double CConfig::GetLoad_Value ( string  val_index)

Get the force value at an load boundary.

Parameters
[in]val_index- Index corresponding to the load boundary.
Returns
The load value.

Definition at line 8338 of file config_structure.cpp.

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◆ GetLocationStations()

su2double CConfig::GetLocationStations ( unsigned short  val_section)
inline

Get the airfoil sections in the slicing process.

Parameters
[in]val_section- Index of the section.
Returns
Coordinate of the airfoil to slice.

Definition at line 803 of file config_structure.inl.

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◆ GetLow_MemoryOutput()

bool CConfig::GetLow_MemoryOutput ( void  )
inline

Get information about writing a volume solution file.

Returns
TRUE means that a volume solution file will be written.

Definition at line 1647 of file config_structure.inl.

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◆ GetMach()

su2double CConfig::GetMach ( void  )
inline

Get the value of the Mach number (velocity divided by speed of sound).

Returns
Value of the Mach number.

Definition at line 434 of file config_structure.inl.

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◆ GetMach_Motion()

su2double CConfig::GetMach_Motion ( void  )
inline

Get the mach number based on the mesh velocity and freestream quantities.

Returns
Mach number based on the mesh velocity and freestream quantities.

Definition at line 910 of file config_structure.inl.

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◆ GetMarker_ActDiskInlet_TagBound()

string CConfig::GetMarker_ActDiskInlet_TagBound ( unsigned short  val_marker)
inline

Get the index of the surface defined in the geometry file.

Parameters
[in]val_marker- Value of the marker in which we are interested.
Returns
Value of the index that is in the geometry file for the surface that has the marker val_marker.

Definition at line 1304 of file config_structure.inl.

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◆ GetMarker_ActDiskOutlet_TagBound()

string CConfig::GetMarker_ActDiskOutlet_TagBound ( unsigned short  val_marker)
inline

Get the index of the surface defined in the geometry file.

Parameters
[in]val_marker- Value of the marker in which we are interested.
Returns
Value of the index that is in the geometry file for the surface that has the marker val_marker.

Definition at line 1306 of file config_structure.inl.

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◆ GetMarker_All_Analyze()

unsigned short CConfig::GetMarker_All_Analyze ( unsigned short  val_marker)
inline

Get the plotting information for a marker val_marker.

Parameters
[in]val_marker- 0 or 1 depending if the the marker is going to be moved.
Returns
0 or 1 depending if the marker is going to be plotted.

Definition at line 1375 of file config_structure.inl.

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◆ GetMarker_All_Designing()

unsigned short CConfig::GetMarker_All_Designing ( unsigned short  val_marker)
inline

Get the design information for a marker val_marker.

Parameters
[in]val_marker- 0 or 1 depending if the the marker is going to be monitored.
Returns
0 or 1 depending if the marker is going to be monitored.

Definition at line 1367 of file config_structure.inl.

◆ GetMarker_All_DV()

unsigned short CConfig::GetMarker_All_DV ( unsigned short  val_marker)
inline

Get the DV information for a marker val_marker.

Parameters
[in]val_marker- 0 or 1 depending if the the marker is going to be affected by design variables.
Returns
0 or 1 depending if the marker is going to be affected by design variables.

Definition at line 1387 of file config_structure.inl.

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◆ GetMarker_All_GeoEval()

unsigned short CConfig::GetMarker_All_GeoEval ( unsigned short  val_marker)
inline

Get the monitoring information for a marker val_marker.

Parameters
[in]val_marker- 0 or 1 depending if the the marker is going to be monitored.
Returns
0 or 1 depending if the marker is going to be monitored.

Definition at line 1365 of file config_structure.inl.

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◆ GetMarker_All_KindBC()

unsigned short CConfig::GetMarker_All_KindBC ( unsigned short  val_marker)
inline

Get the kind of boundary for each marker.

Parameters
[in]val_marker- Index of the marker in which we are interested.
Returns
Kind of boundary for the marker val_marker.

Definition at line 1329 of file config_structure.inl.

◆ GetMarker_All_MixingPlaneInterface()

unsigned short CConfig::GetMarker_All_MixingPlaneInterface ( unsigned short  val_marker)
inline

Get the MixingPlane interface information for a marker val_marker.

Parameters
[in]val_markervalue of the marker on the grid.
Returns
0 if is not part of the MixingPlane Interface and greater than 1 if it is part.

Definition at line 1385 of file config_structure.inl.

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◆ GetMarker_All_Monitoring()

unsigned short CConfig::GetMarker_All_Monitoring ( unsigned short  val_marker)
inline

Get the monitoring information for a marker val_marker.

Parameters
[in]val_marker- 0 or 1 depending if the the marker is going to be monitored.
Returns
0 or 1 depending if the marker is going to be monitored.

Definition at line 1363 of file config_structure.inl.

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◆ GetMarker_All_Moving()

unsigned short CConfig::GetMarker_All_Moving ( unsigned short  val_marker)
inline

Get the motion information for a marker val_marker.

Parameters
[in]val_marker- 0 or 1 depending if the the marker is going to be moved.
Returns
0 or 1 depending if the marker is going to be moved.

Definition at line 1389 of file config_structure.inl.

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◆ GetMarker_All_PerBound()

short CConfig::GetMarker_All_PerBound ( unsigned short  val_marker)
inline

Get an internal index that identify the periodic boundary conditions.

Parameters
[in]val_marker- Value of the marker that correspond with the periodic boundary.
Returns
The internal index of the periodic boundary condition.

Definition at line 1361 of file config_structure.inl.

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◆ GetMarker_All_Plotting()

unsigned short CConfig::GetMarker_All_Plotting ( unsigned short  val_marker)
inline

Get the plotting information for a marker val_marker.

Parameters
[in]val_marker- 0 or 1 depending if the the marker is going to be moved.
Returns
0 or 1 depending if the marker is going to be plotted.

Definition at line 1373 of file config_structure.inl.

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◆ GetMarker_All_PyCustom()

unsigned short CConfig::GetMarker_All_PyCustom ( unsigned short  val_marker)
inline

Get the Python customization for a marker val_marker.

Parameters
[in]val_marker- Index of the marker in which we are interested.
Returns
0 or 1 depending if the marker is going to be customized in Python.

Definition at line 1391 of file config_structure.inl.

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◆ GetMarker_All_SendRecv()

short CConfig::GetMarker_All_SendRecv ( unsigned short  val_marker)
inline

Get the send-receive information for a marker val_marker.

Parameters
[in]val_marker- 0 or 1 depending if the the marker is going to be moved.
Returns
If positive, the information is sended to that domain, in case negative the information is receive from that domain.

Definition at line 1369 of file config_structure.inl.

◆ GetMarker_All_TagBound() [1/2]

short CConfig::GetMarker_All_TagBound ( string  val_tag)
inline

Get the tag if the iMarker defined in the geometry file.

Parameters
[in]val_tag- Value of the tag in which we are interested.
Returns
Value of the marker val_marker that is in the geometry file for the surface that has the tag.

Definition at line 1322 of file config_structure.inl.

◆ GetMarker_All_TagBound() [2/2]

string CConfig::GetMarker_All_TagBound ( unsigned short  val_marker)
inline

Get the index of the surface defined in the geometry file.

Parameters
[in]val_marker- Value of the marker in which we are interested.
Returns
Value of the index that is in the geometry file for the surface that has the marker val_marker.

Definition at line 1302 of file config_structure.inl.

◆ GetMarker_All_Turbomachinery()

unsigned short CConfig::GetMarker_All_Turbomachinery ( unsigned short  val_marker)
inline

Get the Turbomachinery information for a marker val_marker.

Parameters
[in]val_markervalue of the marker on the grid.
Returns
0 if is not part of the Turbomachinery and greater than 1 if it is part.

Definition at line 1381 of file config_structure.inl.

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◆ GetMarker_All_TurbomachineryFlag()

unsigned short CConfig::GetMarker_All_TurbomachineryFlag ( unsigned short  val_marker)
inline

Get the Turbomachinery flag information for a marker val_marker.

Parameters
[in]val_markervalue of the marker on the grid.
Returns
0 if is not part of the Turbomachinery, flag INFLOW or OUTFLOW if it is part.

Definition at line 1383 of file config_structure.inl.

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◆ GetMarker_All_ZoneInterface()

unsigned short CConfig::GetMarker_All_ZoneInterface ( unsigned short  val_marker)
inline

Get the FSI interface information for a marker val_marker.

Parameters
[in]val_marker- 0 or 1 depending if the the marker is going to be moved.
Returns
0 or 1 depending if the marker is part of the FSI interface.

Definition at line 1377 of file config_structure.inl.

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◆ GetMarker_Analyze_TagBound()

string CConfig::GetMarker_Analyze_TagBound ( unsigned short  val_marker)
inline

Get the name of the surface defined in the geometry file.

Parameters
[in]val_marker- Value of the marker in which we are interested.
Returns
Name that is in the geometry file for the surface that has the marker val_marker.

Definition at line 1320 of file config_structure.inl.

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◆ GetMarker_CfgFile_ActDiskOutlet()

unsigned short CConfig::GetMarker_CfgFile_ActDiskOutlet ( string  val_marker)

Get Actuator Disk Outlet for boundary val_marker (actuator disk inlet).

Returns
Actuator Disk Outlet from the config information for the marker val_marker.

Definition at line 7543 of file config_structure.cpp.

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◆ GetMarker_CfgFile_Analyze()

unsigned short CConfig::GetMarker_CfgFile_Analyze ( string  val_marker)

Get the plotting information from the config definition for the marker val_marker.

Returns
Plotting information of the boundary in the config information for the marker val_marker.

Definition at line 6511 of file config_structure.cpp.

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◆ GetMarker_CfgFile_Designing()

unsigned short CConfig::GetMarker_CfgFile_Designing ( string  val_marker)

Get the monitoring information from the config definition for the marker val_marker.

Returns
Monitoring information of the boundary in the config information for the marker val_marker.

Definition at line 6497 of file config_structure.cpp.

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◆ GetMarker_CfgFile_DV()

unsigned short CConfig::GetMarker_CfgFile_DV ( string  val_marker)

Get the DV information from the config definition for the marker val_marker.

Returns
DV information of the boundary in the config information for the marker val_marker.

Definition at line 6547 of file config_structure.cpp.

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◆ GetMarker_CfgFile_EngineExhaust()

unsigned short CConfig::GetMarker_CfgFile_EngineExhaust ( string  val_marker)

Get Actuator Disk Outlet for boundary val_marker (actuator disk inlet).

Returns
Actuator Disk Outlet from the config information for the marker val_marker.

Definition at line 7559 of file config_structure.cpp.

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◆ GetMarker_CfgFile_GeoEval()

unsigned short CConfig::GetMarker_CfgFile_GeoEval ( string  val_marker)

Get the monitoring information from the config definition for the marker val_marker.

Returns
Monitoring information of the boundary in the config information for the marker val_marker.

Definition at line 6490 of file config_structure.cpp.

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◆ GetMarker_CfgFile_KindBC()

unsigned short CConfig::GetMarker_CfgFile_KindBC ( string  val_marker)

Get the boundary information (kind of boundary) in the config information of the marker val_marker.

Returns
Kind of boundary in the config information of the marker val_marker.

Definition at line 6476 of file config_structure.cpp.

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◆ GetMarker_CfgFile_MixingPlaneInterface()

unsigned short CConfig::GetMarker_CfgFile_MixingPlaneInterface ( string  val_marker)

Get the MixingPlane interface information from the config definition for the marker val_marker.

Returns
Plotting information of the boundary in the config information for the marker val_marker.

Definition at line 6540 of file config_structure.cpp.

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◆ GetMarker_CfgFile_Monitoring()

unsigned short CConfig::GetMarker_CfgFile_Monitoring ( string  val_marker)

Get the monitoring information from the config definition for the marker val_marker.

Returns
Monitoring information of the boundary in the config information for the marker val_marker.

Definition at line 6483 of file config_structure.cpp.

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◆ GetMarker_CfgFile_Moving()

unsigned short CConfig::GetMarker_CfgFile_Moving ( string  val_marker)

Get the motion information from the config definition for the marker val_marker.

Returns
Motion information of the boundary in the config information for the marker val_marker.

Definition at line 6554 of file config_structure.cpp.

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◆ GetMarker_CfgFile_PerBound()

unsigned short CConfig::GetMarker_CfgFile_PerBound ( string  val_marker)

Get the periodic information from the config definition of the marker val_marker.

Returns
Periodic information of the boundary in the config information of the marker val_marker.

Definition at line 6568 of file config_structure.cpp.

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◆ GetMarker_CfgFile_Plotting()

unsigned short CConfig::GetMarker_CfgFile_Plotting ( string  val_marker)

Get the plotting information from the config definition for the marker val_marker.

Returns
Plotting information of the boundary in the config information for the marker val_marker.

Definition at line 6504 of file config_structure.cpp.

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◆ GetMarker_CfgFile_PyCustom()

unsigned short CConfig::GetMarker_CfgFile_PyCustom ( string  val_marker)

Get the Python customization information from the config definition for the marker val_marker.

Returns
Python customization information of the boundary in the config information for the marker val_marker.

Definition at line 6561 of file config_structure.cpp.

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◆ GetMarker_CfgFile_TagBound() [1/2]

unsigned short CConfig::GetMarker_CfgFile_TagBound ( string  val_marker)

Get the index in the config information of the marker val_marker.

Note
When we read the config file, it stores the markers in a particular vector.
Returns
Index in the config information of the marker val_marker.

Definition at line 6460 of file config_structure.cpp.

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◆ GetMarker_CfgFile_TagBound() [2/2]

string CConfig::GetMarker_CfgFile_TagBound ( unsigned short  val_marker)

Get the name in the config information of the marker number val_marker.

Note
When we read the config file, it stores the markers in a particular vector.
Returns
Name of the marker in the config information of the marker val_marker.

Definition at line 6472 of file config_structure.cpp.

◆ GetMarker_CfgFile_Turbomachinery()

unsigned short CConfig::GetMarker_CfgFile_Turbomachinery ( string  val_marker)

Get the TurboPerformance information from the config definition for the marker val_marker.

Returns
TurboPerformance information of the boundary in the config information for the marker val_marker.

Definition at line 6526 of file config_structure.cpp.

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◆ GetMarker_CfgFile_TurbomachineryFlag()

unsigned short CConfig::GetMarker_CfgFile_TurbomachineryFlag ( string  val_marker)

Get the TurboPerformance flag information from the config definition for the marker val_marker.

Returns
TurboPerformance flag information of the boundary in the config information for the marker val_marker.

Definition at line 6533 of file config_structure.cpp.

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◆ GetMarker_CfgFile_ZoneInterface()

unsigned short CConfig::GetMarker_CfgFile_ZoneInterface ( string  val_marker)

Get the FSI interface information from the config definition for the marker val_marker.

Returns
Plotting information of the boundary in the config information for the marker val_marker.

Definition at line 6519 of file config_structure.cpp.

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◆ GetMarker_EngineExhaust_TagBound()

string CConfig::GetMarker_EngineExhaust_TagBound ( unsigned short  val_marker)
inline

Get the index of the surface defined in the geometry file.

Parameters
[in]val_marker- Value of the marker in which we are interested.
Returns
Value of the index that is in the geometry file for the surface that has the marker val_marker.

Definition at line 1310 of file config_structure.inl.

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◆ GetMarker_EngineInflow_TagBound()

string CConfig::GetMarker_EngineInflow_TagBound ( unsigned short  val_marker)
inline

Get the index of the surface defined in the geometry file.

Parameters
[in]val_marker- Value of the marker in which we are interested.
Returns
Value of the index that is in the geometry file for the surface that has the marker val_marker.

Definition at line 1308 of file config_structure.inl.

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◆ GetMarker_HeatFlux_TagBound()

string CConfig::GetMarker_HeatFlux_TagBound ( unsigned short  val_marker)
inline

Get the name of the surface defined in the geometry file.

Parameters
[in]val_marker- Value of the marker in which we are interested.
Returns
Name that is in the geometry file for the surface that has the marker val_marker.

Definition at line 1314 of file config_structure.inl.

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◆ GetMarker_Monitoring_TagBound()

string CConfig::GetMarker_Monitoring_TagBound ( unsigned short  val_marker)
inline

Get the name of the surface defined in the geometry file.

Parameters
[in]val_marker- Value of the marker in which we are interested.
Returns
Name that is in the geometry file for the surface that has the marker val_marker.

Definition at line 1312 of file config_structure.inl.

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◆ GetMarker_Moving()

unsigned short CConfig::GetMarker_Moving ( string  val_marker)

Get the internal index for a moving boundary val_marker.

Returns
Internal index for a moving boundary val_marker.

Definition at line 7593 of file config_structure.cpp.

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◆ GetMarker_Moving_TagBound()

string CConfig::GetMarker_Moving_TagBound ( unsigned short  val_marker)
inline

Get the name of the surface defined in the geometry file.

Parameters
[in]val_marker- Value of the marker in which we are interested.
Returns
Name that is in the geometry file for the surface that has the marker val_marker.

Definition at line 1316 of file config_structure.inl.

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◆ GetMarker_n_ZoneInterface()

unsigned short CConfig::GetMarker_n_ZoneInterface ( void  )
inline

Get the number of FSI interface markers val_marker.

Parameters
[in]void.
Returns
Number of markers belonging to the FSI interface.

Definition at line 1379 of file config_structure.inl.

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◆ GetMarker_PerBound()

string CConfig::GetMarker_PerBound ( unsigned short  val_marker)
inline

get outlet bounds name for Turbomachinery performance calculation.

Returns
name of the bound.

Definition at line 1262 of file config_structure.inl.

◆ GetMarker_Periodic_Donor()

unsigned short CConfig::GetMarker_Periodic_Donor ( string  val_marker)

Get the rotationally periodic donor marker for boundary val_marker.

Returns
Periodic donor marker from the config information for the marker val_marker.

Definition at line 7413 of file config_structure.cpp.

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◆ GetMarker_PyCustom_TagBound()

string CConfig::GetMarker_PyCustom_TagBound ( unsigned short  val_marker)
inline

Get the name of the surface defined in the geometry file.

Parameters
[in]val_marker- Value of the marker in which we are interested.
Returns
Name that is in the geometry file for the surface that has the marker val_marker.

Definition at line 1318 of file config_structure.inl.

◆ GetMarker_Shroud()

string CConfig::GetMarker_Shroud ( unsigned short  val_marker)
inline

Get the marker shroud.

Returns
marker shroud.

Definition at line 1240 of file config_structure.inl.

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◆ GetMarker_TurboPerf_BoundIn()

string CConfig::GetMarker_TurboPerf_BoundIn ( unsigned short  index)
inline

get inlet bounds name for Turbomachinery performance calculation.

Returns
name of the bound.

Definition at line 1258 of file config_structure.inl.

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◆ GetMarker_TurboPerf_BoundOut()

string CConfig::GetMarker_TurboPerf_BoundOut ( unsigned short  index)
inline

get outlet bounds name for Turbomachinery performance calculation.

Returns
name of the bound.

Definition at line 1260 of file config_structure.inl.

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◆ GetMarker_ZoneInterface()

int CConfig::GetMarker_ZoneInterface ( string  val_marker)

Get the name of the marker val_marker.

Returns
The interface which owns that marker val_marker.

Definition at line 6575 of file config_structure.cpp.

◆ GetMassFrac_FreeStream()

su2double * CConfig::GetMassFrac_FreeStream ( void  )
inline

Get the vector of free stream mass fraction values.

Returns
Ratio of species mass to mixture mass.

Definition at line 576 of file config_structure.inl.

◆ GetMatchingMesh()

bool CConfig::GetMatchingMesh ( void  )
inline

Identifies if the mesh is matching or not (temporary, while implementing interpolation procedures).

Returns
TRUE if the mesh is matching, FALSE otherwise.

Definition at line 1809 of file config_structure.inl.

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◆ GetMaterialCompressibility()

unsigned short CConfig::GetMaterialCompressibility ( void  )
inline

Compressibility/incompressibility of the solids analysed using the structural solver.

Returns
Compressible or incompressible.

Definition at line 402 of file config_structure.inl.

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◆ GetMaterialDensity()

su2double CConfig::GetMaterialDensity ( unsigned short  id_val)
inline

Get the Material Density.

Returns
Value of the Material Density.

Definition at line 394 of file config_structure.inl.

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◆ GetMaterialModel()

unsigned short CConfig::GetMaterialModel ( void  )
inline

Compressibility/incompressibility of the solids analysed using the structural solver.

Returns
Compressible or incompressible.

Definition at line 404 of file config_structure.inl.

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◆ GetMax_DeltaTime()

su2double CConfig::GetMax_DeltaTime ( void  )
inline

Get the Courant Friedrich Levi number for unsteady simulations.

Returns
CFL number for unsteady simulations.

Definition at line 763 of file config_structure.inl.

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◆ GetMax_Vel2()

su2double CConfig::GetMax_Vel2 ( void  )
inline

Get the maximum velocity^2 in the domain for the incompressible preconditioner.

Returns
Value of the maximum velocity^2 in the domain for the incompressible preconditioner.

Definition at line 1945 of file config_structure.inl.

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◆ GetmaxTurkelBeta()

su2double CConfig::GetmaxTurkelBeta ( )
inline

Get the minimum value of Beta for Roe-Turkel preconditioner.

Returns
the minimum value of Beta for Roe-Turkel preconditioner

Definition at line 976 of file config_structure.inl.

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◆ GetMesh_FileFormat()

unsigned short CConfig::GetMesh_FileFormat ( void  )
inline

Get the format of the input/output grid.

Returns
Format of the input/output grid.

Definition at line 1433 of file config_structure.inl.

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◆ GetMesh_FileName()

string CConfig::GetMesh_FileName ( void  )
inline

Get name of the input grid.

Returns
File name of the input grid.

Definition at line 1429 of file config_structure.inl.

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◆ GetMesh_Out_FileName()

string CConfig::GetMesh_Out_FileName ( void  )
inline

Get name of the output grid, this parameter is important for grid adaptation and deformation.

Returns
File name of the output grid.

Definition at line 1431 of file config_structure.inl.

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◆ GetMG_CorrecSmooth()

unsigned short CConfig::GetMG_CorrecSmooth ( unsigned short  val_mesh)
inline

Get the number of implicit Jacobi smoothings of the correction in a multigrid strategy.

Parameters
[in]val_mesh- Index of the grid.
Returns
Number of implicit smoothing iterations.

Definition at line 829 of file config_structure.inl.

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◆ GetMG_PostSmooth()

unsigned short CConfig::GetMG_PostSmooth ( unsigned short  val_mesh)
inline

Get the number of post-smoothings in a multigrid strategy.

Parameters
[in]val_mesh- Index of the grid.
Returns
Number of smoothing iterations.

Definition at line 824 of file config_structure.inl.

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◆ GetMG_PreSmooth()

unsigned short CConfig::GetMG_PreSmooth ( unsigned short  val_mesh)
inline

Get the number of pre-smoothings in a multigrid strategy.

Parameters
[in]val_mesh- Index of the grid.
Returns
Number of smoothing iterations.

Definition at line 819 of file config_structure.inl.

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◆ GetMGCycle()

unsigned short CConfig::GetMGCycle ( void  )
inline

Get the kind of multigrid (V or W).

Note
This variable is used in a recursive way to perform the different kind of cycles
Returns
0 or 1 depending of we are dealing with a V or W cycle.

Definition at line 751 of file config_structure.inl.

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◆ GetMinLogResidual()

su2double CConfig::GetMinLogResidual ( void  )
inline

Value of the minimum residual value (log10 scale).

Returns
Value of the minimum residual value (log10 scale).

Definition at line 1531 of file config_structure.inl.

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◆ GetMinLogResidual_BGS_F()

su2double CConfig::GetMinLogResidual_BGS_F ( void  )
inline

Value of the minimum flow residual value for BGS applications (log10 scale).

Returns
Value of the minimum residual value (log10 scale).

Definition at line 1893 of file config_structure.inl.

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◆ GetMinLogResidual_BGS_S()

su2double CConfig::GetMinLogResidual_BGS_S ( void  )
inline

Value of the minimum flow residual value for BGS applications (log10 scale).

Returns
Value of the minimum residual value (log10 scale).

Definition at line 1897 of file config_structure.inl.

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◆ GetMinLogResidualFSI()

su2double CConfig::GetMinLogResidualFSI ( void  )
inline

Value of the minimum residual value for FSI applications (log10 scale).

Returns
Value of the minimum residual value (log10 scale).

Definition at line 1889 of file config_structure.inl.

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◆ GetminTurkelBeta()

su2double CConfig::GetminTurkelBeta ( )
inline

Get the minimum value of Beta for Roe-Turkel preconditioner.

Returns
the minimum value of Beta for Roe-Turkel preconditioner

Definition at line 974 of file config_structure.inl.

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◆ GetMixedout_Coeff()

su2double CConfig::GetMixedout_Coeff ( unsigned short  iCoeff)
inline

Get mixedout coefficients.

Returns
mixedout coefficient.

Definition at line 1204 of file config_structure.inl.

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◆ GetModVel_FreeStream()

su2double CConfig::GetModVel_FreeStream ( void  )
inline

Get the value of the frestream temperature.

Returns
Freestream temperature.

Definition at line 494 of file config_structure.inl.

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◆ GetModVel_FreeStreamND()

su2double CConfig::GetModVel_FreeStreamND ( void  )
inline

Get the value of the frestream temperature.

Returns
Freestream temperature.

Definition at line 496 of file config_structure.inl.

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◆ GetMolar_Mass() [1/2]

su2double CConfig::GetMolar_Mass ( unsigned short  iSpecies)

Provides the molar mass of each species present in multi species fluid.

Returns
: Mass of each species in Kg

◆ GetMolar_Mass() [2/2]

su2double* CConfig::GetMolar_Mass ( void  )

Provides the molar mass of each species present in multi species fluid.

Returns
: Vector of molar mass of each species in kg/kmol

◆ GetMolecular_Weight()

su2double CConfig::GetMolecular_Weight ( void  )
inline

Get the value of the molecular weight for an incompressible ideal gas (g/mol).

Returns
Value of the molecular weight for an incompressible ideal gas (g/mol).

Definition at line 450 of file config_structure.inl.

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◆ GetMonitorOutletPressure()

su2double CConfig::GetMonitorOutletPressure ( void  )
inline

Get final Outlet Pressure value for the ramp.

Returns
Monitor Outlet Pressure value.

Definition at line 1198 of file config_structure.inl.

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◆ GetMotion_Origin_X()

su2double CConfig::GetMotion_Origin_X ( unsigned short  val_iZone)
inline

Get x-coordinate of the mesh motion origin.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
X-coordinate of the mesh motion origin.

Definition at line 912 of file config_structure.inl.

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◆ GetMotion_Origin_Y()

su2double CConfig::GetMotion_Origin_Y ( unsigned short  val_iZone)
inline

Get y-coordinate of the mesh motion origin.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Y-coordinate of the mesh motion origin.

Definition at line 914 of file config_structure.inl.

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◆ GetMotion_Origin_Z()

su2double CConfig::GetMotion_Origin_Z ( unsigned short  val_iZone)
inline

Get z-coordinate of the mesh motion origin.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Z-coordinate of the mesh motion origin.

Definition at line 916 of file config_structure.inl.

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◆ GetMoveMotion_Origin()

unsigned short CConfig::GetMoveMotion_Origin ( unsigned short  val_marker)
inline

Get if we should update the motion origin.

Parameters
[in]val_marker- Value of the marker in which we are interested.
Returns
yes or no to update motion origin.

Definition at line 972 of file config_structure.inl.

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◆ GetMPICommunicator()

SU2_MPI::Comm CConfig::GetMPICommunicator ( )

Get the MPI communicator of SU2.

Returns
MPI communicator of SU2.

Definition at line 152 of file config_structure.cpp.

◆ GetMu_Constant()

su2double CConfig::GetMu_Constant ( void  )
inline

Get the value of the constant viscosity.

Returns
Constant viscosity.

Definition at line 876 of file config_structure.inl.

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◆ GetMu_ConstantND()

su2double CConfig::GetMu_ConstantND ( void  )
inline

Get the value of the non-dimensional constant viscosity.

Returns
Non-dimensional constant viscosity.

Definition at line 878 of file config_structure.inl.

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◆ GetMu_Ref()

su2double CConfig::GetMu_Ref ( void  )
inline

Get the value of the reference viscosity for Sutherland model.

Returns
The reference viscosity.

Definition at line 884 of file config_structure.inl.

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◆ GetMu_RefND()

su2double CConfig::GetMu_RefND ( void  )
inline

Get the value of the non-dimensional reference viscosity for Sutherland model.

Returns
The non-dimensional reference viscosity.

Definition at line 886 of file config_structure.inl.

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◆ GetMu_S()

su2double CConfig::GetMu_S ( void  )
inline

Get the value of the reference S for Sutherland model.

Returns
The reference S.

Definition at line 892 of file config_structure.inl.

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◆ GetMu_SND()

su2double CConfig::GetMu_SND ( void  )
inline

Get the value of the non-dimensional reference S for Sutherland model.

Returns
The non-dimensional reference S.

Definition at line 894 of file config_structure.inl.

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◆ GetMu_Temperature_Ref()

su2double CConfig::GetMu_Temperature_Ref ( void  )
inline

Get the value of the reference temperature for Sutherland model.

Returns
The reference temperature.

Definition at line 888 of file config_structure.inl.

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◆ GetMu_Temperature_RefND()

su2double CConfig::GetMu_Temperature_RefND ( void  )
inline

Get the value of the non-dimensional reference temperature for Sutherland model.

Returns
The non-dimensional reference temperature.

Definition at line 890 of file config_structure.inl.

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◆ GetMultiInstance_FileName()

string CConfig::GetMultiInstance_FileName ( string  val_filename,
int  val_iInst 
)

Append the instance index to the restart or the solution files.

Returns
Name of the restart file for the flow variables.

Definition at line 7111 of file config_structure.cpp.

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◆ GetMultiInstance_HistoryFileName()

string CConfig::GetMultiInstance_HistoryFileName ( string  val_filename,
int  val_iInst 
)

Append the instance index to the restart or the solution files.

Returns
Name of the restart file for the flow variables.

Definition at line 7124 of file config_structure.cpp.

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◆ GetMultizone_FileName()

string CConfig::GetMultizone_FileName ( string  val_filename,
int  val_iZone 
)

Append the zone index to the restart or the solution files.

Returns
Name of the restart file for the flow variables.

Definition at line 7083 of file config_structure.cpp.

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◆ GetMultizone_HistoryFileName()

string CConfig::GetMultizone_HistoryFileName ( string  val_filename,
int  val_iZone 
)

Append the zone index to the restart or the solution files.

Returns
Name of the restart file for the flow variables.

Definition at line 7097 of file config_structure.cpp.

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◆ GetMUSCL()

bool CConfig::GetMUSCL ( void  )
inline

Get if the upwind scheme used MUSCL or not.

Note
This is the information that the code will use, the method will change in runtime depending of the specific equation (direct, adjoint, linearized) that is being solved.
Returns
MUSCL scheme.

Definition at line 1070 of file config_structure.inl.

◆ GetMUSCL_AdjFlow()

bool CConfig::GetMUSCL_AdjFlow ( void  )
inline

Get if the upwind scheme used MUSCL or not.

Note
This is the information that the code will use, the method will change in runtime depending of the specific equation (direct, adjoint, linearized) that is being solved.
Returns
MUSCL scheme.

Definition at line 1078 of file config_structure.inl.

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◆ GetMUSCL_AdjTurb()

bool CConfig::GetMUSCL_AdjTurb ( void  )
inline

Get if the upwind scheme used MUSCL or not.

Note
This is the information that the code will use, the method will change in runtime depending of the specific equation (direct, adjoint, linearized) that is being solved.
Returns
MUSCL scheme.

Definition at line 1080 of file config_structure.inl.

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◆ GetMUSCL_Flow()

bool CConfig::GetMUSCL_Flow ( void  )
inline

Get if the upwind scheme used MUSCL or not.

Note
This is the information that the code will use, the method will change in runtime depending of the specific equation (direct, adjoint, linearized) that is being solved.
Returns
MUSCL scheme.

Definition at line 1072 of file config_structure.inl.

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◆ GetMUSCL_Heat()

bool CConfig::GetMUSCL_Heat ( void  )
inline

Get if the upwind scheme used MUSCL or not.

Note
This is the information that the code will use, the method will change in runtime depending of the specific equation (direct, adjoint, linearized) that is being solved.
Returns
MUSCL scheme.

Definition at line 1076 of file config_structure.inl.

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◆ GetMUSCL_Turb()

bool CConfig::GetMUSCL_Turb ( void  )
inline

Get if the upwind scheme used MUSCL or not.

Note
This is the information that the code will use, the method will change in runtime depending of the specific equation (direct, adjoint, linearized) that is being solved.
Returns
MUSCL scheme.

Definition at line 1074 of file config_structure.inl.

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◆ GetNacelleLocation()

su2double CConfig::GetNacelleLocation ( unsigned short  val_index)
inline

Get the defintion of the nacelle location.

Parameters
[in]val_index- Index of the section.
Returns
Coordinate of the nacelle location.

Definition at line 805 of file config_structure.inl.

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◆ GetnBlades()

su2double CConfig::GetnBlades ( unsigned short  val_iZone)
inline

number Turbomachinery blades computed using the pitch information.

Returns
nBlades.

Definition at line 1226 of file config_structure.inl.

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◆ GetnDiatomics()

unsigned short CConfig::GetnDiatomics ( void  )

Retrieves the number of monatomic species in the multicomponent gas.

Returns
: Number of monatomic species.

◆ GetnDim()

unsigned short CConfig::GetnDim ( string  val_mesh_filename,
unsigned short  val_format 
)
static

Gets the number of dimensions in the mesh file.

Parameters
[in]val_mesh_filename- Name of the file with the grid information.
[in]val_format- Format of the file with the grid information.
Returns
Total number of domains in the grid file.

Definition at line 246 of file config_structure.cpp.

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◆ GetnDim_Electric_Field()

unsigned short CConfig::GetnDim_Electric_Field ( void  )
inline

Get the dimensionality of the electric field.

Returns
Number of integration coefficients.

Definition at line 1837 of file config_structure.inl.

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◆ GetnDV()

unsigned short CConfig::GetnDV ( void  )
inline

Get the number of design variables.

Returns
Number of the design variables.

Definition at line 775 of file config_structure.inl.

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◆ GetnDV_Value()

unsigned short CConfig::GetnDV_Value ( unsigned short  iDV)
inline

Get the number of design variables.

Returns
Number of the design variables.

Definition at line 777 of file config_structure.inl.

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◆ GetnElasticityMod()

unsigned short CConfig::GetnElasticityMod ( void  )
inline

Get the number of different values for the elasticity modulus.

Returns
Number of different values for the elasticity modulus.

Definition at line 396 of file config_structure.inl.

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◆ GetnElectric_Constant()

unsigned short CConfig::GetnElectric_Constant ( void  )
inline

Get the number of different electric constants.

Returns
Value of the DE modulus.

Definition at line 368 of file config_structure.inl.

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◆ GetnElectric_Field()

unsigned short CConfig::GetnElectric_Field ( void  )
inline

Get the number of different values for the modulus of the electric field.

Returns
Number of different values for the modulus of the electric field.

Definition at line 1835 of file config_structure.inl.

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◆ GetnElStates()

unsigned short* CConfig::GetnElStates ( void  )

Provides number electron states for calculating e_el.

Returns
: Vector of number of electron states for each species

◆ GetNew_Elem_Adapt()

su2double CConfig::GetNew_Elem_Adapt ( void  )
inline

Get the number of new elements added in the adaptation process.

Returns
percentage of new elements that are going to be added in the adaptation.

Definition at line 1060 of file config_structure.inl.

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◆ GetNewmark_beta()

su2double CConfig::GetNewmark_beta ( void  )
inline

Get Newmark alpha parameter.

Returns
Value of the Newmark alpha parameter.

Definition at line 1827 of file config_structure.inl.

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◆ GetNewmark_gamma()

su2double CConfig::GetNewmark_gamma ( void  )
inline

Get Newmark delta parameter.

Returns
Value of the Newmark delta parameter.

Definition at line 1829 of file config_structure.inl.

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◆ GetnExtIter()

unsigned long CConfig::GetnExtIter ( void  )
inline

Get the number of external iterations.

Returns
Number of external iterations.

Definition at line 294 of file config_structure.inl.

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◆ GetnFFD_Fix_IDir()

unsigned short CConfig::GetnFFD_Fix_IDir ( void  )
inline

Get the number of planes to fix in the I direction.

Returns
Number of planes to fix in the I direction.

Definition at line 807 of file config_structure.inl.

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◆ GetnFFD_Fix_JDir()

unsigned short CConfig::GetnFFD_Fix_JDir ( void  )
inline

Get the number of planes to fix in the J direction.

Returns
Number of planes to fix in the J direction.

Definition at line 809 of file config_structure.inl.

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◆ GetnFFD_Fix_KDir()

unsigned short CConfig::GetnFFD_Fix_KDir ( void  )
inline

Get the number of planes to fix in the K direction.

Returns
Number of planes to fix in the K direction.

Definition at line 811 of file config_structure.inl.

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◆ GetnFFD_Iter()

unsigned short CConfig::GetnFFD_Iter ( void  )
inline

Get the number of iterations to evaluate the parametric coordinates.

Returns
Number of iterations to evaluate the parametric coordinates.

Definition at line 1735 of file config_structure.inl.

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◆ GetnFFDBox()

unsigned short CConfig::GetnFFDBox ( void  )
inline

Get the number of FFD boxes.

Returns
Number of FFD boxes.

Definition at line 779 of file config_structure.inl.

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◆ GetnID_DV()

unsigned short CConfig::GetnID_DV ( void  )
inline

Get the ID for the FEA region that we want to compute the gradient for using direct differentiation.

Returns
ID

Definition at line 1873 of file config_structure.inl.

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◆ GetnInc_Inlet()

unsigned short CConfig::GetnInc_Inlet ( void  )
inline

Get the total number of types in Kind_Inc_Inlet list.

Returns
Total number of types in Kind_Inc_Inlet list

Definition at line 1172 of file config_structure.inl.

◆ GetnIntCoeffs()

unsigned short CConfig::GetnIntCoeffs ( void  )
inline

Get the number of integration coefficients provided by the user.

Returns
Number of integration coefficients.

Definition at line 1831 of file config_structure.inl.

◆ GetnIterFSI()

unsigned short CConfig::GetnIterFSI ( void  )
inline

Get the number of fluid subiterations roblems.

Returns
Number of FSI subiters.

Definition at line 1795 of file config_structure.inl.

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◆ GetnIterFSI_Ramp()

unsigned short CConfig::GetnIterFSI_Ramp ( void  )
inline

Get the number of subiterations while a ramp is applied.

Returns
Number of FSI subiters.

Definition at line 1797 of file config_structure.inl.

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◆ GetnLevels_TimeAccurateLTS()

unsigned short CConfig::GetnLevels_TimeAccurateLTS ( void  )
inline

Get the number of time levels for time accurate local time stepping.

Returns
Number of time levels.

Definition at line 787 of file config_structure.inl.

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◆ GetnLocationStations()

unsigned short CConfig::GetnLocationStations ( void  )
inline

Get the number of sections.

Returns
Number of sections

Definition at line 1264 of file config_structure.inl.

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◆ GetnMarker_ActDiskInlet()

unsigned short CConfig::GetnMarker_ActDiskInlet ( void  )
inline

Get the total number of boundary markers.

Returns
Total number of boundary markers.

Definition at line 1419 of file config_structure.inl.

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◆ GetnMarker_ActDiskOutlet()

unsigned short CConfig::GetnMarker_ActDiskOutlet ( void  )
inline

Get the total number of boundary markers.

Returns
Total number of boundary markers.

Definition at line 1421 of file config_structure.inl.

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◆ GetnMarker_All()

unsigned short CConfig::GetnMarker_All ( void  )
inline

Get the total number of boundary markers.

Returns
Total number of boundary markers.

Definition at line 1393 of file config_structure.inl.

◆ GetnMarker_Analyze()

unsigned short CConfig::GetnMarker_Analyze ( void  )
inline

Get the total number of moving markers.

Returns
Total number of moving markers.

Definition at line 1415 of file config_structure.inl.

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◆ GetnMarker_DV()

unsigned short CConfig::GetnMarker_DV ( void  )
inline

Get the total number of DV markers.

Returns
Total number of DV markers.

Definition at line 1409 of file config_structure.inl.

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◆ GetnMarker_EngineExhaust()

unsigned short CConfig::GetnMarker_EngineExhaust ( void  )
inline

Get the total number of boundary markers.

Returns
Total number of boundary markers.

Definition at line 1399 of file config_structure.inl.

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◆ GetnMarker_EngineInflow()

unsigned short CConfig::GetnMarker_EngineInflow ( void  )
inline

Get the total number of boundary markers.

Returns
Total number of boundary markers.

Definition at line 1397 of file config_structure.inl.

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◆ GetnMarker_Fluid_InterfaceBound()

unsigned short CConfig::GetnMarker_Fluid_InterfaceBound ( void  )
inline

Get the total number of boundary markers.

Returns
Total number of boundary markers.

Definition at line 1403 of file config_structure.inl.

◆ GetnMarker_HeatFlux()

unsigned short CConfig::GetnMarker_HeatFlux ( void  )
inline

Get the total number of heat flux markers.

Returns
Total number of heat flux markers.

Definition at line 1425 of file config_structure.inl.

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◆ GetnMarker_InterfaceBound()

unsigned short CConfig::GetnMarker_InterfaceBound ( void  )
inline

Get the total number of boundary markers.

Returns
Total number of boundary markers.

Definition at line 1401 of file config_structure.inl.

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◆ GetnMarker_Max()

unsigned short CConfig::GetnMarker_Max ( void  )
inline

Get the total number of boundary markers.

Returns
Total number of boundary markers.

Definition at line 1395 of file config_structure.inl.

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◆ GetnMarker_MixingPlaneInterface()

unsigned short CConfig::GetnMarker_MixingPlaneInterface ( void  )
inline

number mixing plane interface specified from config file.

Returns
number of bound.

Definition at line 1234 of file config_structure.inl.

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◆ GetnMarker_Monitoring()

unsigned short CConfig::GetnMarker_Monitoring ( void  )
inline

Get the total number of monitoring markers.

Returns
Total number of monitoring markers.

Definition at line 1407 of file config_structure.inl.

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◆ GetnMarker_Moving()

unsigned short CConfig::GetnMarker_Moving ( void  )
inline

Get the total number of moving markers.

Returns
Total number of moving markers.

Definition at line 1411 of file config_structure.inl.

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◆ GetnMarker_NearFieldBound()

unsigned short CConfig::GetnMarker_NearFieldBound ( void  )
inline

Get the total number of boundary markers.

Returns
Total number of boundary markers.

Definition at line 1417 of file config_structure.inl.

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◆ GetnMarker_Periodic()

unsigned short CConfig::GetnMarker_Periodic ( void  )
inline

Get the total number of periodic markers.

Returns
Total number of periodic markers.

Definition at line 1423 of file config_structure.inl.

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◆ GetnMarker_PyCustom()

unsigned short CConfig::GetnMarker_PyCustom ( void  )
inline

Get the total number of Python customizable markers.

Returns
Total number of Python customizable markers.

Definition at line 1413 of file config_structure.inl.

◆ GetnMarker_Shroud()

unsigned short CConfig::GetnMarker_Shroud ( void  )
inline

Get number of shroud markers.

Returns
number of marker shroud.

Definition at line 1238 of file config_structure.inl.

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◆ GetnMarker_Transpiration()

unsigned short CConfig::GetnMarker_Transpiration ( void  )
inline

Get the total number of transpiration markers.

Returns
Total number of moving markers.

Definition at line 1405 of file config_structure.inl.

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◆ GetnMarker_Turbomachinery()

unsigned short CConfig::GetnMarker_Turbomachinery ( void  )
inline

number Turbomachinery performance option specified from config file.

Returns
number of bound.

Definition at line 1236 of file config_structure.inl.

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◆ GetnMarker_TurboPerformance()

unsigned short CConfig::GetnMarker_TurboPerformance ( void  )
inline

number Turbomachinery performance option specified from config file.

Returns
number of bound.

Definition at line 1242 of file config_structure.inl.

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◆ GetnMaterialDensity()

unsigned short CConfig::GetnMaterialDensity ( void  )
inline

Get the number of different values for the Material density.

Returns
Number of different values for the Material density.

Definition at line 400 of file config_structure.inl.

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◆ GetnMGLevels()

unsigned short CConfig::GetnMGLevels ( void  )
inline

Get the number of multigrid levels.

Returns
Number of multigrid levels (without including the original grid).

Definition at line 727 of file config_structure.inl.

◆ GetnMonatomics()

unsigned short CConfig::GetnMonatomics ( void  )

Retrieves the number of monatomic species in the multicomponent gas.

Returns
: Number of monatomic species.

◆ GetnObj()

unsigned short CConfig::GetnObj ( void  )
inline

Get the total number of objectives in kind_objective list.

Returns
Total number of objectives in kind_objective list

Definition at line 1427 of file config_structure.inl.

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◆ GetNonphysical_Points()

unsigned long CConfig::GetNonphysical_Points ( void  )
inline

Get the current number of non-physical nodes in the solution.

Returns
Current number of non-physical points.

Definition at line 1785 of file config_structure.inl.

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◆ GetNonphysical_Reconstr()

unsigned long CConfig::GetNonphysical_Reconstr ( void  )
inline

Get the current number of non-physical reconstructions for 2nd-order upwinding.

Returns
Current number of non-physical reconstructions for 2nd-order upwinding.

Definition at line 1789 of file config_structure.inl.

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◆ GetnPeriodicIndex()

unsigned short CConfig::GetnPeriodicIndex ( void  )
inline

Get the total number of SEND_RECEIVE periodic transformations.

Returns
Total number of transformations.

Definition at line 1621 of file config_structure.inl.

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◆ GetnPoissonRatio()

unsigned short CConfig::GetnPoissonRatio ( void  )
inline

Get the number of different values for the Poisson ratio.

Returns
Number of different values for the Poisson ratio.

Definition at line 398 of file config_structure.inl.

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◆ GetnReactions()

unsigned short CConfig::GetnReactions ( void  )

Provides the number of chemical reactions in the chemistry model.

Returns
: The number of chemical reactions, read from input file

◆ GetnRKStep()

unsigned short CConfig::GetnRKStep ( void  )
inline

Get the number of Runge-Kutta steps.

Returns
Number of Runge-Kutta steps.

Definition at line 785 of file config_structure.inl.

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◆ GetnSpan_iZones()

unsigned short CConfig::GetnSpan_iZones ( unsigned short  iZone)
inline

set number span-wise sections to compute 3D BC and performance for turbomachinery.

Definition at line 1256 of file config_structure.inl.

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◆ GetnSpanMaxAllZones()

unsigned short CConfig::GetnSpanMaxAllZones ( void  )
inline

number span-wise sections to compute performance for turbomachinery.

Returns
number of max span-wise sections.

Definition at line 1252 of file config_structure.inl.

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◆ GetnSpanWiseSections()

unsigned short CConfig::GetnSpanWiseSections ( void  )
inline

number span-wise sections to compute 3D BC and performance for turbomachinery.

Returns
number of span-wise sections.

Definition at line 1246 of file config_structure.inl.

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◆ GetnStartUpIter()

unsigned short CConfig::GetnStartUpIter ( void  )
inline

Get the start up iterations using the fine grid, this works only for multigrid problems.

Returns
Start up iterations using the fine grid.

Definition at line 580 of file config_structure.inl.

◆ GetnTimeDOFsADER_DG()

unsigned short CConfig::GetnTimeDOFsADER_DG ( void  )
inline

Get the number time DOFs for ADER-DG.

Returns
Number of time DOFs used in ADER-DG.

Definition at line 791 of file config_structure.inl.

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◆ GetnTimeInstances()

unsigned short CConfig::GetnTimeInstances ( void  )
inline

Retrieves the number of periodic time instances for Harmonic Balance.

Returns
: Number of periodic time instances for Harmonic Balance.

Definition at line 296 of file config_structure.inl.

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◆ GetnTimeIntegrationADER_DG()

unsigned short CConfig::GetnTimeIntegrationADER_DG ( void  )
inline

Get the number time integration points for ADER-DG.

Returns
Number of time integration points used in ADER-DG.

Definition at line 795 of file config_structure.inl.

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◆ GetNuFactor_Engine()

su2double CConfig::GetNuFactor_Engine ( void  )
inline

Get the value of the non-dimensionalized engine turbulence intensity.

Returns
Non-dimensionalized engine intensity.

Definition at line 562 of file config_structure.inl.

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◆ GetNuFactor_FreeStream()

su2double CConfig::GetNuFactor_FreeStream ( void  )
inline

Get the value of the non-dimensionalized freestream turbulence intensity.

Returns
Non-dimensionalized freestream intensity.

Definition at line 560 of file config_structure.inl.

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◆ GetNumberIncrements()

unsigned long CConfig::GetNumberIncrements ( void  )
inline

Get the number of increments for an incremental load.

Returns
Number of increments.

Definition at line 1863 of file config_structure.inl.

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◆ GetnVar()

unsigned short CConfig::GetnVar ( void  )

Provides the number of varaibles.

Returns
Number of variables.

◆ GetnWingStations()

unsigned short CConfig::GetnWingStations ( void  )
inline

Get the number of sections for computing internal volume.

Returns
Number of sections for computing internal volume.

Definition at line 1266 of file config_structure.inl.

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◆ GetnZone() [1/2]

unsigned short CConfig::GetnZone ( string  val_mesh_filename,
unsigned short  val_format,
CConfig config 
)
static

Gets the number of zones in the mesh file.

Parameters
[in]val_mesh_filename- Name of the file with the grid information.
[in]val_format- Format of the file with the grid information.
[in]config- Definition of the particular problem.
Returns
Total number of zones in the grid file.

Definition at line 164 of file config_structure.cpp.

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◆ GetnZone() [2/2]

unsigned short CConfig::GetnZone ( void  )
inline

Provides the number of varaibles.

Returns
Number of variables.

Definition at line 278 of file config_structure.inl.

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◆ GetObjFunc_Extension()

string CConfig::GetObjFunc_Extension ( string  val_filename)

Append the input filename string with the appropriate objective function extension.

Parameters
[in]val_filename- String value of the base filename.
Returns
Name of the file with the appropriate objective function extension.

Definition at line 7137 of file config_structure.cpp.

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◆ GetObjFunc_Grad_FileName()

string CConfig::GetObjFunc_Grad_FileName ( void  )
inline

Get the name of the file with the gradient of the objective function.

Returns
Name of the file with the gradient of the objective function.

Definition at line 1479 of file config_structure.inl.

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◆ GetObjFunc_Value_FileName()

string CConfig::GetObjFunc_Value_FileName ( void  )
inline

Get the name of the file with the gradient of the objective function.

Returns
Name of the file with the gradient of the objective function.

Definition at line 1481 of file config_structure.inl.

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◆ GetOmega_FreeStream()

su2double CConfig::GetOmega_FreeStream ( void  )
inline

Get the value of the non-dimensionalized freestream viscosity.

Returns
Non-dimensionalized freestream viscosity.

Definition at line 558 of file config_structure.inl.

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◆ GetOmega_FreeStreamND()

su2double CConfig::GetOmega_FreeStreamND ( void  )
inline

Get the value of the non-dimensionalized freestream viscosity.

Returns
Non-dimensionalized freestream viscosity.

Definition at line 554 of file config_structure.inl.

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◆ GetOmega_HB()

su2double * CConfig::GetOmega_HB ( void  )
inline

Get the Harmonic Balance frequency pointer.

Returns
Harmonic Balance Frequency pointer.

Definition at line 970 of file config_structure.inl.

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◆ GetOmega_Ref()

su2double CConfig::GetOmega_Ref ( void  )
inline

Get the value of the reference angular velocity for non-dimensionalization.

Returns
Reference angular velocity for non-dimensionalization.

Definition at line 532 of file config_structure.inl.

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◆ GetOpt_LineSearch_Bound()

su2double CConfig::GetOpt_LineSearch_Bound ( void  )
inline

Get the bound for the line search.

Returns
Bound for the line search.

Definition at line 1739 of file config_structure.inl.

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◆ GetOpt_RelaxFactor()

su2double CConfig::GetOpt_RelaxFactor ( void  )
inline

Get the scale factor for the line search.

Returns
Scale factor for the line search.

Definition at line 1741 of file config_structure.inl.

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◆ GetOrderMagResidual()

su2double CConfig::GetOrderMagResidual ( void  )
inline

Value of the order of magnitude reduction of the residual.

Returns
Value of the order of magnitude reduction of the residual.

Definition at line 1529 of file config_structure.inl.

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◆ GetOrderMagResidual_BGS_F()

su2double CConfig::GetOrderMagResidual_BGS_F ( void  )
inline

Value of the order of magnitude reduction of the flow residual for BGS applications.

Returns
Value of the order of magnitude reduction of the residual.

Definition at line 1891 of file config_structure.inl.

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◆ GetOrderMagResidual_BGS_S()

su2double CConfig::GetOrderMagResidual_BGS_S ( void  )
inline

Value of the order of magnitude reduction of the flow residual for BGS applications.

Returns
Value of the order of magnitude reduction of the residual.

Definition at line 1895 of file config_structure.inl.

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◆ GetOrderMagResidualFSI()

su2double CConfig::GetOrderMagResidualFSI ( void  )
inline

Value of the order of magnitude reduction of the residual for FSI applications.

Returns
Value of the order of magnitude reduction of the residual.

Definition at line 1887 of file config_structure.inl.

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◆ GetOutlet_Pressure()

su2double CConfig::GetOutlet_Pressure ( string  val_index)

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 7691 of file config_structure.cpp.

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◆ GetOutput_FileFormat()

unsigned short CConfig::GetOutput_FileFormat ( void  )
inline

Get the format of the output solution.

Returns
Format of the output solution.

Definition at line 1435 of file config_structure.inl.

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◆ GetParamDV()

su2double CConfig::GetParamDV ( unsigned short  val_dv,
unsigned short  val_param 
)
inline

Get a parameter of the particular design variable.

Parameters
[in]val_dv- Number of the design variable that we want to read.
[in]val_param- Index of the parameter that we want to read.
Returns
Design variable parameter.

Definition at line 765 of file config_structure.inl.

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◆ GetPeriodic()

bool CConfig::GetPeriodic ( string  val_mesh_filename,
unsigned short  val_format,
CConfig config 
)
static

Determine whether there are periodic BCs in the grid.

Parameters
[in]val_mesh_filename- Name of the file with the grid information.
[in]val_format- Format of the file with the grid information.
[in]config- Definition of the particular problem.
Returns
Boolean for whether or not there are periodic BCs in the grid.

Definition at line 344 of file config_structure.cpp.

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◆ GetPeriodicCenter()

su2double * CConfig::GetPeriodicCenter ( unsigned short  val_index)
inline

Get the rotation center for a periodic transformation.

Parameters
[in]val_index- Index corresponding to the periodic transformation.
Returns
A vector containing coordinates of the center point.

Definition at line 1623 of file config_structure.inl.

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◆ GetPeriodicRotAngles()

su2double * CConfig::GetPeriodicRotAngles ( string  val_marker)

Angles of rotation for a rotational periodic boundary.

Definition at line 7399 of file config_structure.cpp.

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◆ GetPeriodicRotation()

su2double * CConfig::GetPeriodicRotation ( unsigned short  val_index)
inline

Get the rotation angles for a periodic transformation.

Parameters
[in]val_index- Index corresponding to the periodic transformation.
Returns
A vector containing the angles of rotation.

Definition at line 1629 of file config_structure.inl.

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◆ GetPeriodicRotCenter()

su2double * CConfig::GetPeriodicRotCenter ( string  val_marker)

Center of rotation for a rotational periodic boundary.

Definition at line 7392 of file config_structure.cpp.

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◆ GetPeriodicTranslate()

su2double * CConfig::GetPeriodicTranslate ( unsigned short  val_index)
inline

Get the translation vector for a periodic transformation.

Parameters
[in]val_index- Index corresponding to the periodic transformation.
Returns
The translation vector.

Definition at line 1635 of file config_structure.inl.

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◆ GetPeriodicTranslation()

su2double * CConfig::GetPeriodicTranslation ( string  val_marker)

Translation vector for a rotational periodic boundary.

Definition at line 7406 of file config_structure.cpp.

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◆ GetPitching_Ampl_X()

su2double CConfig::GetPitching_Ampl_X ( unsigned short  val_iZone)
inline

Get the pitching amplitude about the x-axis.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Pitching amplitude about the x-axis.

Definition at line 946 of file config_structure.inl.

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◆ GetPitching_Ampl_Y()

su2double CConfig::GetPitching_Ampl_Y ( unsigned short  val_iZone)
inline

Get the pitching amplitude about the y-axis.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Pitching amplitude about the y-axis.

Definition at line 948 of file config_structure.inl.

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◆ GetPitching_Ampl_Z()

su2double CConfig::GetPitching_Ampl_Z ( unsigned short  val_iZone)
inline

Get the pitching amplitude about the z-axis.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Pitching amplitude about the z-axis.

Definition at line 950 of file config_structure.inl.

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◆ GetPitching_Omega_X()

su2double CConfig::GetPitching_Omega_X ( unsigned short  val_iZone)
inline

Get the angular frequency of a mesh pitching about the x-axis.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Angular frequency of a mesh pitching about the x-axis.

Definition at line 940 of file config_structure.inl.

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◆ GetPitching_Omega_Y()

su2double CConfig::GetPitching_Omega_Y ( unsigned short  val_iZone)
inline

Get the angular frequency of a mesh pitching about the y-axis.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Angular frequency of a mesh pitching about the y-axis.

Definition at line 942 of file config_structure.inl.

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◆ GetPitching_Omega_Z()

su2double CConfig::GetPitching_Omega_Z ( unsigned short  val_iZone)
inline

Get the angular frequency of a mesh pitching about the z-axis.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Angular frequency of a mesh pitching about the z-axis.

Definition at line 944 of file config_structure.inl.

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◆ GetPitching_Phase_X()

su2double CConfig::GetPitching_Phase_X ( unsigned short  val_iZone)
inline

Get the pitching phase offset about the x-axis.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Pitching phase offset about the x-axis.

Definition at line 952 of file config_structure.inl.

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◆ GetPitching_Phase_Y()

su2double CConfig::GetPitching_Phase_Y ( unsigned short  val_iZone)
inline

Get the pitching phase offset about the y-axis.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Pitching phase offset about the y-axis.

Definition at line 954 of file config_structure.inl.

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◆ GetPitching_Phase_Z()

su2double CConfig::GetPitching_Phase_Z ( unsigned short  val_iZone)
inline

Get the pitching phase offset about the z-axis.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Pitching phase offset about the z-axis.

Definition at line 956 of file config_structure.inl.

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◆ GetPlaneTag()

string CConfig::GetPlaneTag ( unsigned short  index)
inline

Get index of the upper and lower horizontal plane.

Parameters
[in]index- 0 means upper surface, and 1 means lower surface.
Returns
Index of the upper and lower surface.

Definition at line 330 of file config_structure.inl.

◆ GetPlot_Section_Forces()

bool CConfig::GetPlot_Section_Forces ( void  )
inline

Get information about writing sectional force files.

Returns
TRUE means that sectional force files will be written for specified markers.

Definition at line 1677 of file config_structure.inl.

◆ GetPlunging_Ampl_X()

su2double CConfig::GetPlunging_Ampl_X ( unsigned short  val_iZone)
inline

Get the plunging amplitude in the x-direction.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Plunging amplitude in the x-direction.

Definition at line 964 of file config_structure.inl.

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◆ GetPlunging_Ampl_Y()

su2double CConfig::GetPlunging_Ampl_Y ( unsigned short  val_iZone)
inline

Get the plunging amplitude in the y-direction.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Plunging amplitude in the y-direction.

Definition at line 966 of file config_structure.inl.

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◆ GetPlunging_Ampl_Z()

su2double CConfig::GetPlunging_Ampl_Z ( unsigned short  val_iZone)
inline

Get the plunging amplitude in the z-direction.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Plunging amplitude in the z-direction.

Definition at line 968 of file config_structure.inl.

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◆ GetPlunging_Omega_X()

su2double CConfig::GetPlunging_Omega_X ( unsigned short  val_iZone)
inline

Get the angular frequency of a mesh plunging in the x-direction.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Angular frequency of a mesh plunging in the x-direction.

Definition at line 958 of file config_structure.inl.

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◆ GetPlunging_Omega_Y()

su2double CConfig::GetPlunging_Omega_Y ( unsigned short  val_iZone)
inline

Get the angular frequency of a mesh plunging in the y-direction.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Angular frequency of a mesh plunging in the y-direction.

Definition at line 960 of file config_structure.inl.

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◆ GetPlunging_Omega_Z()

su2double CConfig::GetPlunging_Omega_Z ( unsigned short  val_iZone)
inline

Get the angular frequency of a mesh plunging in the z-direction.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Angular frequency of a mesh plunging in the z-direction.

Definition at line 962 of file config_structure.inl.

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◆ GetPnormHeat()

su2double CConfig::GetPnormHeat ( void  )

Get the p-norm for heat-flux objective functions (adjoint problem).

Returns
Value of the heat flux p-norm

◆ GetPoissonRatio()

su2double CConfig::GetPoissonRatio ( unsigned short  id_val)
inline

Get the Poisson's ratio.

Returns
Value of the Poisson's ratio.

Definition at line 392 of file config_structure.inl.

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◆ GetPoissonSolver()

bool CConfig::GetPoissonSolver ( void  )
inline

Get information about the poisson solver condition.

Returns
TRUE if it is a poisson solver condition; otherwise FALSE.

Definition at line 1585 of file config_structure.inl.

◆ GetPosition_Plane()

su2double CConfig::GetPosition_Plane ( void  )
inline

Value of the position of the Near Field (y coordinate for 2D, and z coordinate for 3D).

Returns
Value of the Near Field position.

Definition at line 1541 of file config_structure.inl.

◆ GetPrandtl_Lam()

su2double CConfig::GetPrandtl_Lam ( void  )
inline

Get the value of the laminar Prandtl number.

Returns
Laminar Prandtl number.

Definition at line 504 of file config_structure.inl.

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◆ GetPrandtl_Turb()

su2double CConfig::GetPrandtl_Turb ( void  )
inline

Get the value of the turbulent Prandtl number.

Returns
Turbulent Prandtl number.

Definition at line 506 of file config_structure.inl.

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◆ GetPredictorOrder()

unsigned short CConfig::GetPredictorOrder ( void  )
inline

Get the order of the predictor for FSI applications.

Returns
Order of predictor

Definition at line 1859 of file config_structure.inl.

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◆ GetPressure_Critical()

su2double CConfig::GetPressure_Critical ( void  )
inline

Get the value of the critical pressure.

Returns
Critical pressure.

Definition at line 866 of file config_structure.inl.

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◆ GetPressure_FreeStream()

su2double CConfig::GetPressure_FreeStream ( void  )
inline

Get the value of the non-dimensionalized freestream pressure.

Returns
Non-dimensionalized freestream pressure.

Definition at line 498 of file config_structure.inl.

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◆ GetPressure_FreeStreamND()

su2double CConfig::GetPressure_FreeStreamND ( void  )
inline

Get the value of the non-dimensionalized freestream pressure.

Returns
Non-dimensionalized freestream pressure.

Definition at line 536 of file config_structure.inl.

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◆ GetPressure_Ref()

su2double CConfig::GetPressure_Ref ( void  )
inline

Get the value of the reference pressure for non-dimensionalization.

Returns
Reference pressure for non-dimensionalization.

Definition at line 512 of file config_structure.inl.

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◆ GetPressure_Thermodynamic()

su2double CConfig::GetPressure_Thermodynamic ( void  )
inline

Get the value of the thermodynamic pressure.

Returns
Thermodynamic pressure.

Definition at line 500 of file config_structure.inl.

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◆ GetPressure_ThermodynamicND()

su2double CConfig::GetPressure_ThermodynamicND ( void  )
inline

Get the value of the non-dimensionalized thermodynamic pressure.

Returns
Non-dimensionalized thermodynamic pressure.

Definition at line 538 of file config_structure.inl.

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◆ GetPressureOut_BC()

su2double CConfig::GetPressureOut_BC ( )

Get the outlet pressure imposed as BC for internal flow.

Returns
outlet pressure

Definition at line 7784 of file config_structure.cpp.

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◆ GetPrestretch()

bool CConfig::GetPrestretch ( void  )
inline

Decide whether it's necessary to read a reference geometry.

Returns
TRUE if it's necessary to read a reference geometry, FALSE otherwise.

Definition at line 408 of file config_structure.inl.

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◆ GetPrestretch_FEMFileName()

string CConfig::GetPrestretch_FEMFileName ( void  )
inline

Get the name of the file with the reference geometry of the structural problem.

Returns
Name of the file with the reference geometry of the structural problem.

Definition at line 416 of file config_structure.inl.

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◆ GetPseudoStatic()

bool CConfig::GetPseudoStatic ( void  )
inline

Identifies if the mesh is matching or not (temporary, while implementing interpolation procedures).

Returns
TRUE if the mesh is matching, FALSE otherwise.

Definition at line 1807 of file config_structure.inl.

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◆ GetQCR()

bool CConfig::GetQCR ( void  )
inline

Get QCR (SA-QCR2000).

Definition at line 1959 of file config_structure.inl.

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◆ GetQuadrature_Factor_Curved()

su2double CConfig::GetQuadrature_Factor_Curved ( void  )
inline

Get the factor applied during quadrature of curved elements.

Returns
The specified curved element quadrature factor.

Definition at line 1917 of file config_structure.inl.

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◆ GetQuadrature_Factor_Straight()

su2double CConfig::GetQuadrature_Factor_Straight ( void  )
inline

Get the factor applied during quadrature of straight elements.

Returns
The specified straight element quadrature factor.

Definition at line 1915 of file config_structure.inl.

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◆ GetQuadrature_Factor_Time_ADER_DG()

su2double CConfig::GetQuadrature_Factor_Time_ADER_DG ( void  )
inline

Get the factor applied during time quadrature for ADER-DG.

Returns
The specified ADER-DG time quadrature factor.

Definition at line 1919 of file config_structure.inl.

◆ GetRadialBasisFunctionParameter()

su2double CConfig::GetRadialBasisFunctionParameter ( void  )
inline

Get the basis function radius to use for radial basis function interpolation for FSI.

Definition at line 1881 of file config_structure.inl.

◆ GetRadialBasisFunctionPolynomialOption()

bool CConfig::GetRadialBasisFunctionPolynomialOption ( void  )
inline

Get option of whether to use polynomial terms in Radial Basis Function interpolation.

Definition at line 1879 of file config_structure.inl.

◆ GetRamp_Load()

bool CConfig::GetRamp_Load ( void  )
inline

Check if the user wants to apply the load as a ramp.

Returns
TRUE means that the load is to be applied as a ramp.

Definition at line 1845 of file config_structure.inl.

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◆ GetRamp_Time()

su2double CConfig::GetRamp_Time ( void  )
inline

Get the maximum time of the ramp.

Returns
Value of the max time while the load is linearly increased

Definition at line 1847 of file config_structure.inl.

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◆ GetRampAndRelease_Load()

bool CConfig::GetRampAndRelease_Load ( void  )
inline

Check if the user wants to apply the load as a ramp.

Returns
TRUE means that the load is to be applied as a ramp.

Definition at line 1849 of file config_structure.inl.

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◆ GetRampOutletPressure()

bool CConfig::GetRampOutletPressure ( void  )
inline

Get Outlet Pressure Ramp option.

Returns
Ramp Outlet pressure option.

Definition at line 1202 of file config_structure.inl.

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◆ GetRampOutletPressure_Coeff()

su2double CConfig::GetRampOutletPressure_Coeff ( unsigned short  iCoeff)
inline

Get coeff for Outlet Pressure Ramp.

Returns
coeff Ramp Outlet Pressure.

Definition at line 1194 of file config_structure.inl.

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◆ GetRampRotatingFrame()

bool CConfig::GetRampRotatingFrame ( void  )
inline

Get Rotating Frame Ramp option.

Returns
Ramp Rotating Frame option.

Definition at line 1192 of file config_structure.inl.

◆ GetRampRotatingFrame_Coeff()

su2double CConfig::GetRampRotatingFrame_Coeff ( unsigned short  iCoeff)
inline

Get coeff for Rotating Frame Ramp.

Returns
coeff Ramp Rotating Frame.

Definition at line 1190 of file config_structure.inl.

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◆ GetRead_Binary_Restart()

bool CConfig::GetRead_Binary_Restart ( void  )
inline

Flag for whether binary SU2 native restart files are read.

Returns
Flag for whether binary SU2 native restart files are read, if TRUE then the code will load binary restart files.

Definition at line 1290 of file config_structure.inl.

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◆ GetRef_Inc_NonDim()

unsigned short CConfig::GetRef_Inc_NonDim ( void  )
inline

Get the kind of incompressible non-dimensionalization.

Returns
Kind of incompressible non-dimensionalization.

Definition at line 286 of file config_structure.inl.

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◆ GetRef_NonDim()

unsigned short CConfig::GetRef_NonDim ( void  )
inline

Get the kind of non-dimensionalization.

Returns
Kind of non-dimensionalization.

Definition at line 284 of file config_structure.inl.

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◆ GetRefArea()

su2double CConfig::GetRefArea ( void  )
inline

Get the reference area for non dimensional coefficient computation. If the value from the is 0 then, the code will compute the reference area using the projection of the shape into the z plane (3D) or the x plane (2D).

Returns
Value of the reference area for coefficient computation.

Definition at line 356 of file config_structure.inl.

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◆ GetRefElemLength()

su2double CConfig::GetRefElemLength ( void  )
inline

Get the reference element length for computing the slope limiting epsilon.

Returns
Reference element length for slope limiting epsilon.

Definition at line 420 of file config_structure.inl.

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◆ GetRefGeom()

bool CConfig::GetRefGeom ( void  )
inline

Decide whether it's necessary to read a reference geometry.

Returns
TRUE if it's necessary to read a reference geometry, FALSE otherwise.

Definition at line 384 of file config_structure.inl.

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◆ GetRefGeom_FEMFileName()

string CConfig::GetRefGeom_FEMFileName ( void  )
inline

Get the name of the file with the reference geometry of the structural problem.

Returns
Name of the file with the reference geometry of the structural problem.

Definition at line 386 of file config_structure.inl.

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◆ GetRefGeom_FileFormat()

unsigned short CConfig::GetRefGeom_FileFormat ( void  )
inline

Get the format of the reference geometry file.

Returns
Format of the reference geometry file.

Definition at line 388 of file config_structure.inl.

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◆ GetRefGeom_Penalty()

su2double CConfig::GetRefGeom_Penalty ( void  )
inline

Get the penalty weight value for the objective function.

Returns
Penalty weight value for the reference geometry objective function.

Definition at line 1855 of file config_structure.inl.

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◆ GetRefLength()

su2double CConfig::GetRefLength ( void  )
inline

Get the reference length for computing moment (the default value is 1).

Returns
Reference length for moment computation.

Definition at line 418 of file config_structure.inl.

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◆ GetRefNode_Displacement()

su2double CConfig::GetRefNode_Displacement ( unsigned short  val_coeff)
inline

Get the values for the reference node displacement.

Parameters
[in]val_coeff- Index of the displacement.

Definition at line 380 of file config_structure.inl.

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◆ GetRefNode_ID()

unsigned long CConfig::GetRefNode_ID ( void  )
inline

Get the ID of the reference node.

Returns
Number of FSI subiters.

Definition at line 378 of file config_structure.inl.

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◆ GetRefNode_Penalty()

su2double CConfig::GetRefNode_Penalty ( void  )
inline

Get the penalty weight value for the objective function.

Returns
Penalty weight value for the reference geometry objective function.

Definition at line 382 of file config_structure.inl.

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◆ GetRefOriginMoment()

su2double * CConfig::GetRefOriginMoment ( unsigned short  val_marker)
inline

Get reference origin for moment computation.

Parameters
[in]val_marker- the marker we are monitoring.
Returns
Reference origin (in cartesians coordinates) for moment computation.

Definition at line 582 of file config_structure.inl.

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◆ GetRefOriginMoment_X()

su2double CConfig::GetRefOriginMoment_X ( unsigned short  val_marker)
inline

Get reference origin x-coordinate for moment computation.

Parameters
[in]val_marker- the marker we are monitoring.
Returns
Reference origin x-coordinate (in cartesians coordinates) for moment computation.

Definition at line 591 of file config_structure.inl.

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◆ GetRefOriginMoment_Y()

su2double CConfig::GetRefOriginMoment_Y ( unsigned short  val_marker)
inline

Get reference origin y-coordinate for moment computation.

Parameters
[in]val_marker- the marker we are monitoring.
Returns
Reference origin y-coordinate (in cartesians coordinates) for moment computation.

Definition at line 593 of file config_structure.inl.

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◆ GetRefOriginMoment_Z()

su2double CConfig::GetRefOriginMoment_Z ( unsigned short  val_marker)
inline

Get reference origin z-coordinate for moment computation.

Parameters
[in]val_marker- the marker we are monitoring.
Returns
Reference origin z-coordinate (in cartesians coordinates) for moment computation.

Definition at line 595 of file config_structure.inl.

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◆ GetRefSharpEdges()

su2double CConfig::GetRefSharpEdges ( void  )
inline

Get the reference coefficient for detecting sharp edges.

Returns
Reference coefficient for detecting sharp edges.

Definition at line 422 of file config_structure.inl.

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◆ GetRefTemperature()

su2double* CConfig::GetRefTemperature ( void  )

Provides the thermodynamic reference temperatures from the JANAF tables.

Returns
: Vector of reference temperatures [K]

◆ GetRelaxation_Factor_AdjFlow()

su2double CConfig::GetRelaxation_Factor_AdjFlow ( void  )
inline

Get the relaxation coefficient of the linear solver for the implicit formulation.

Returns
relaxation coefficient of the linear solver for the implicit formulation.

Definition at line 1004 of file config_structure.inl.

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◆ GetRelaxation_Factor_CHT()

su2double CConfig::GetRelaxation_Factor_CHT ( void  )
inline

Get the relaxation coefficient of the CHT coupling.

Returns
relaxation coefficient of the CHT coupling.

Definition at line 1008 of file config_structure.inl.

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◆ GetRelaxation_Factor_Flow()

su2double CConfig::GetRelaxation_Factor_Flow ( void  )
inline

Get the relaxation coefficient of the linear solver for the implicit formulation.

Returns
relaxation coefficient of the linear solver for the implicit formulation.

Definition at line 1002 of file config_structure.inl.

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◆ GetRelaxation_Factor_Turb()

su2double CConfig::GetRelaxation_Factor_Turb ( void  )
inline

Get the relaxation coefficient of the linear solver for the implicit formulation.

Returns
relaxation coefficient of the linear solver for the implicit formulation.

Definition at line 1006 of file config_structure.inl.

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◆ GetRelaxation_Method_FSI()

unsigned short CConfig::GetRelaxation_Method_FSI ( void  )
inline

Get the relaxation method chosen for the simulation.

Returns
Value of the relaxation method

Definition at line 1885 of file config_structure.inl.

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◆ GetReorientElements()

bool CConfig::GetReorientElements ( void  )
inline

Get information about element reorientation.

Returns
TRUE means that elements can be reoriented if suspected unhealthy

Definition at line 324 of file config_structure.inl.

◆ GetResidual_Criteria_FEM()

unsigned short CConfig::GetResidual_Criteria_FEM ( void  )
inline

Get the criteria for structural residual (relative/absolute).

Returns
Relative/Absolute criteria for structural convergence.

Definition at line 1491 of file config_structure.inl.

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◆ GetResidual_FEM_ETOL()

su2double CConfig::GetResidual_FEM_ETOL ( void  )
inline

Value of the displacement tolerance UTOL for FEM structural analysis (log10 scale).

Returns
Value of Res_FEM_UTOL (log10 scale).

Definition at line 1903 of file config_structure.inl.

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◆ GetResidual_FEM_RTOL()

su2double CConfig::GetResidual_FEM_RTOL ( void  )
inline

Value of the displacement tolerance UTOL for FEM structural analysis (log10 scale).

Returns
Value of Res_FEM_UTOL (log10 scale).

Definition at line 1901 of file config_structure.inl.

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◆ GetResidual_FEM_UTOL()

su2double CConfig::GetResidual_FEM_UTOL ( void  )
inline

Value of the displacement tolerance UTOL for FEM structural analysis (log10 scale).

Returns
Value of Res_FEM_UTOL (log10 scale).

Definition at line 1899 of file config_structure.inl.

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◆ GetResidual_FileName()

string CConfig::GetResidual_FileName ( void  )

Get the name of the file with the residual of the problem.

Returns
Name of the file with the residual of the problem.

◆ GetResidual_Func_Flow()

unsigned short CConfig::GetResidual_Func_Flow ( void  )
inline

Get functional that is going to be used to evaluate the residual flow convergence.

Returns
Functional that is going to be used to evaluate the residual flow convergence.

Definition at line 1493 of file config_structure.inl.

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◆ GetRestart()

bool CConfig::GetRestart ( void  )
inline

Provides the restart information.

Returns
Restart information, if TRUE then the code will use the solution as restart.

Definition at line 1286 of file config_structure.inl.

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◆ GetRestart_AdjFEMFileName()

string CConfig::GetRestart_AdjFEMFileName ( void  )
inline

Get the name of the restart file for the structural adjoint variables.

Returns
Name of the restart file for the structural adjoint variables.

Definition at line 1475 of file config_structure.inl.

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◆ GetRestart_AdjFileName()

string CConfig::GetRestart_AdjFileName ( void  )
inline

Get the name of the restart file for the adjoint variables (drag objective function).

Returns
Name of the restart file for the adjoint variables (drag objective function).

Definition at line 1471 of file config_structure.inl.

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◆ GetRestart_Bandwidth_Agg()

su2double CConfig::GetRestart_Bandwidth_Agg ( void  )
inline

Set the sum of the bandwidth for writing binary restarts (to be averaged later).

Returns
Sum of the bandwidth for writing binary restarts.

Definition at line 1949 of file config_structure.inl.

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◆ GetRestart_FEMFileName()

string CConfig::GetRestart_FEMFileName ( void  )
inline

Get the name of the restart file for the structural variables.

Returns
Name of the restart file for the structural variables.

Definition at line 1473 of file config_structure.inl.

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◆ GetRestart_Flow()

bool CConfig::GetRestart_Flow ( void  )
inline

For some problems like adjoint or the linearized equations it is necessary to restart the flow solution.

Returns
Flow restart information, if TRUE then the code will restart the flow solution.

Definition at line 1292 of file config_structure.inl.

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◆ GetRestart_FlowFileName()

string CConfig::GetRestart_FlowFileName ( void  )
inline

Get the name of the restart file for the flow variables.

Returns
Name of the restart file for the flow variables.

Definition at line 1467 of file config_structure.inl.

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◆ GetRestart_HeatFileName()

string CConfig::GetRestart_HeatFileName ( void  )
inline

Get the name of the restart file for the heat variables.

Returns
Name of the restart file for the flow variables.

Definition at line 1469 of file config_structure.inl.

◆ GetReynolds()

su2double CConfig::GetReynolds ( void  )
inline

Get the Reynolds number. Dimensionless number that gives a measure of the ratio of inertial forces to viscous forces and consequently quantifies the relative importance of these two types of forces for given flow condition.

Returns
Value of the Reynolds number.

Definition at line 611 of file config_structure.inl.

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◆ GetRiemann_FlowDir()

su2double * CConfig::GetRiemann_FlowDir ( string  val_marker)

Get the Flowdir at Riemann boundary.

Parameters
[in]val_marker- Index corresponding to the Riemann boundary.
Returns
The Flowdir

Definition at line 7719 of file config_structure.cpp.

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◆ GetRiemann_Solver_FEM()

unsigned short CConfig::GetRiemann_Solver_FEM ( void  )
inline

Get the kind of Riemann solver for the DG method (FEM flow solver).

Note
This value is obtained from the config file, and it is constant during the computation.
Returns
Kind of Riemann solver for the DG method (FEM flow solver).

Definition at line 1913 of file config_structure.inl.

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◆ GetRiemann_Var1()

su2double CConfig::GetRiemann_Var1 ( string  val_marker)

Get the var 1 at Riemann boundary.

Parameters
[in]val_marker- Index corresponding to the Riemann boundary.
Returns
The var1

Definition at line 7705 of file config_structure.cpp.

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◆ GetRiemann_Var2()

su2double CConfig::GetRiemann_Var2 ( string  val_marker)

Get the var 2 at Riemann boundary.

Parameters
[in]val_marker- Index corresponding to the Riemann boundary.
Returns
The var2

Definition at line 7712 of file config_structure.cpp.

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◆ GetRoe_Kappa()

su2double CConfig::GetRoe_Kappa ( void  )
inline

Get the relaxation coefficient of the linear solver for the implicit formulation.

Returns
relaxation coefficient of the linear solver for the implicit formulation.

Definition at line 1010 of file config_structure.inl.

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◆ GetRotating_Frame()

bool CConfig::GetRotating_Frame ( void  )
inline

Get information about the rotational frame.

Returns
TRUE if there is a rotational frame; otherwise FALSE.

Definition at line 1579 of file config_structure.inl.

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◆ GetRotation_Rate_X()

su2double CConfig::GetRotation_Rate_X ( unsigned short  val_iZone)
inline

Get the angular velocity of the mesh about the x-axis.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Angular velocity of the mesh about the x-axis.

Definition at line 930 of file config_structure.inl.

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◆ GetRotation_Rate_Y()

su2double CConfig::GetRotation_Rate_Y ( unsigned short  val_iZone)
inline

Get the angular velocity of the mesh about the y-axis.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Angular velocity of the mesh about the y-axis.

Definition at line 932 of file config_structure.inl.

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◆ GetRotation_Rate_Z()

su2double CConfig::GetRotation_Rate_Z ( unsigned short  val_iZone)
inline

Get the angular velocity of the mesh about the z-axis.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Angular velocity of the mesh about the z-axis.

Definition at line 934 of file config_structure.inl.

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◆ GetRotationModes()

su2double* CConfig::GetRotationModes ( void  )

Provides the number of rotational modes of energy storage.

Returns
: Vector of rotational mode count

◆ GetRxnTcb_a()

su2double* CConfig::GetRxnTcb_a ( void  )

Provides the rate controlling temperature exponents for chemistry.

Returns
: Rate controlling temperature exponents.

◆ GetRxnTcb_b()

su2double* CConfig::GetRxnTcb_b ( void  )

Provides the rate controlling temperature exponents for chemistry.

Returns
: Rate controlling temperature exponents.

◆ GetRxnTcf_a()

su2double* CConfig::GetRxnTcf_a ( void  )

Provides the rate controlling temperature exponents for chemistry.

Returns
: Rate controlling temperature exponents.

◆ GetRxnTcf_b()

su2double* CConfig::GetRxnTcf_b ( void  )

Provides the rate controlling temperature exponents for chemistry.

Returns
: Rate controlling temperature exponents.

◆ GetSecondaryFlow_ActDisk()

su2double CConfig::GetSecondaryFlow_ActDisk ( void  )
inline

Get the value of the non-dimensionalized actuator disk turbulence intensity.

Returns
Non-dimensionalized actuator disk intensity.

Definition at line 564 of file config_structure.inl.

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◆ GetSemiSpan()

su2double CConfig::GetSemiSpan ( void  )
inline

Get the wing semi span.

Returns
value of the wing semi span.

Definition at line 1012 of file config_structure.inl.

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◆ GetSens_Remove_Sharp()

bool CConfig::GetSens_Remove_Sharp ( void  )
inline

Provides information about if the sharp edges are going to be removed from the sensitivity.

Returns
FALSE means that the sharp edges will be removed from the sensitivity.

Definition at line 1615 of file config_structure.inl.

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◆ GetSine_Load()

bool CConfig::GetSine_Load ( void  )
inline

Check if the user wants to apply the load as a ramp.

Returns
TRUE means that the load is to be applied as a ramp.

Definition at line 1851 of file config_structure.inl.

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◆ GetSizeMatMulPadding()

unsigned short CConfig::GetSizeMatMulPadding ( void  )
inline

Function to make available the matrix size in vectorization in order to optimize the gemm performance.

Returns
The matrix size in this direction.

Definition at line 1923 of file config_structure.inl.

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◆ GetSmoothNumGrid()

bool CConfig::GetSmoothNumGrid ( void  )
inline

Get information about there is a smoothing of the grid coordinates.

Returns
TRUE if there is smoothing of the grid coordinates; otherwise FALSE.

Definition at line 1597 of file config_structure.inl.

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◆ GetSolution_AdjFEMFileName()

string CConfig::GetSolution_AdjFEMFileName ( void  )
inline

Get the name of the file with the solution of the adjoint structural problem.

Returns
Name of the file with the solution of the structural problem.

Definition at line 1451 of file config_structure.inl.

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◆ GetSolution_AdjFileName()

string CConfig::GetSolution_AdjFileName ( void  )
inline

Get the name of the file with the solution of the adjoint flow problem with drag objective function.

Returns
Name of the file with the solution of the adjoint flow problem with drag objective function.

Definition at line 1447 of file config_structure.inl.

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◆ GetSolution_FEMFileName()

string CConfig::GetSolution_FEMFileName ( void  )
inline

Get the name of the file with the solution of the structural problem.

Returns
Name of the file with the solution of the structural problem.

Definition at line 1449 of file config_structure.inl.

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◆ GetSolution_FlowFileName()

string CConfig::GetSolution_FlowFileName ( void  )
inline

Get the name of the file with the solution of the flow problem.

Returns
Name of the file with the solution of the flow problem.

Definition at line 1445 of file config_structure.inl.

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◆ GetSpatialFourier()

bool CConfig::GetSpatialFourier ( void  )
inline

Verify if there is mixing plane interface specified from config file.

Returns
boolean.

Definition at line 1224 of file config_structure.inl.

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◆ GetSpecific_Heat_Cp()

su2double CConfig::GetSpecific_Heat_Cp ( void  )
inline

Get the value of specific heat at constant pressure.

Returns
Value of the constant: Cp

Definition at line 452 of file config_structure.inl.

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◆ GetSpecific_Heat_Cp_Solid()

su2double CConfig::GetSpecific_Heat_Cp_Solid ( void  )
inline

Get the value of the specific heat for solids.

Returns
Specific heat number (solid).

Definition at line 454 of file config_structure.inl.

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◆ GetSpecific_Heat_CpND()

su2double CConfig::GetSpecific_Heat_CpND ( void  )
inline

Get the non-dimensional value of specific heat at constant pressure.

Returns
Value of the non-dim. constant: Cp

Definition at line 456 of file config_structure.inl.

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◆ GetSpecific_Heat_Cv()

su2double CConfig::GetSpecific_Heat_Cv ( void  )
inline

Get the value of specific heat at constant volume.

Returns
Value of the constant: Cv

Definition at line 458 of file config_structure.inl.

◆ GetSpecific_Heat_CvND()

su2double CConfig::GetSpecific_Heat_CvND ( void  )
inline

Get the non-dimensional value of specific heat at constant volume.

Returns
Value of the non-dim. constant: Cv

Definition at line 460 of file config_structure.inl.

◆ GetSpline()

su2double CConfig::GetSpline ( vector< su2double > &  xa,
vector< su2double > &  ya,
vector< su2double > &  y2a,
unsigned long  n,
su2double  x 
)

Given the arrays xa[1..n] and ya[1..n], which tabulate a function (with the xai’s in order), and given the array y2a[1..n], which is the output from spline above, and given a value of x, this routine returns a cubic-spline interpolated value y. Numerical Recipes: The Art of Scientific Computing, Third Edition in C++.

Returns
The interpolated value of for x.

Definition at line 8457 of file config_structure.cpp.

◆ GetStartConv_Iter()

unsigned long CConfig::GetStartConv_Iter ( void  )
inline

Get the number of iterations that are not considered in the convergence criteria.

Returns
Number of iterations before starting with the convergence criteria.

Definition at line 1501 of file config_structure.inl.

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◆ GetStations_Bounds()

su2double CConfig::GetStations_Bounds ( unsigned short  val_var)
inline

Get the value of the limits for the sections.

Returns
Value of the limits for the sections.

Definition at line 438 of file config_structure.inl.

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◆ GetSteadyRestart()

bool CConfig::GetSteadyRestart ( void  )
inline

Identifies if we want to restart from a steady or an unsteady solution.

Returns
TRUE if we restart from steady state solution, FALSE otherwise.

Definition at line 1811 of file config_structure.inl.

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◆ GetStructure_FileName()

string CConfig::GetStructure_FileName ( void  )
inline

Get the name of the file with the structure variables.

Returns
Name of the file with the structure variables.

Definition at line 1455 of file config_structure.inl.

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◆ GetSubsonicEngine()

bool CConfig::GetSubsonicEngine ( void  )
inline

Divide the rectbles and hexahedron.

Returns
TRUE if the elements must be divided; otherwise FALSE.

Definition at line 1517 of file config_structure.inl.

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◆ GetSubsonicEngine_Cyl()

su2double * CConfig::GetSubsonicEngine_Cyl ( void  )
inline

Get the the coordinates where of the box where a subsonic region is imposed.

Returns
Coordinates where of the box where the grid is going to be a subsonic region.

Definition at line 340 of file config_structure.inl.

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◆ GetSubsonicEngine_Values()

su2double * CConfig::GetSubsonicEngine_Values ( void  )
inline

Get the the coordinates where of the box where a subsonic region is imposed.

Returns
Coordinates where of the box where the grid is going to be a subsonic region.

Definition at line 342 of file config_structure.inl.

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◆ GetSurface_DC60()

su2double CConfig::GetSurface_DC60 ( unsigned short  val_imarker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 214 of file config_structure.inl.

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◆ GetSurface_Density()

su2double CConfig::GetSurface_Density ( unsigned short  val_imarker)
inline

Get the density at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The density.

Definition at line 194 of file config_structure.inl.

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◆ GetSurface_Enthalpy()

su2double CConfig::GetSurface_Enthalpy ( unsigned short  val_imarker)
inline

Get the enthalpy at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The density.

Definition at line 196 of file config_structure.inl.

◆ GetSurface_IDC()

su2double CConfig::GetSurface_IDC ( unsigned short  val_imarker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 216 of file config_structure.inl.

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◆ GetSurface_IDC_Mach()

su2double CConfig::GetSurface_IDC_Mach ( unsigned short  val_imarker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 218 of file config_structure.inl.

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◆ GetSurface_IDR()

su2double CConfig::GetSurface_IDR ( unsigned short  val_imarker)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 220 of file config_structure.inl.

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◆ GetSurface_Mach()

su2double CConfig::GetSurface_Mach ( unsigned short  val_imarker)
inline

Get the mach number at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The mach number.

Definition at line 188 of file config_structure.inl.

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◆ GetSurface_MassFlow()

su2double CConfig::GetSurface_MassFlow ( unsigned short  val_imarker)
inline

Get the massflow at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The massflow.

Definition at line 186 of file config_structure.inl.

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◆ GetSurface_MomentumDistortion()

su2double CConfig::GetSurface_MomentumDistortion ( unsigned short  val_imarker)
inline

Get the momentum distortion at the surface.

Parameters
[in]val_imarker- Index corresponding to the outlet boundary.
Returns
The momentum distortion.

Definition at line 206 of file config_structure.inl.

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◆ GetSurface_NormalVelocity()

su2double CConfig::GetSurface_NormalVelocity ( unsigned short  val_imarker)
inline

Get the normal velocity at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The normal velocity.

Definition at line 198 of file config_structure.inl.

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◆ GetSurface_Pressure()

su2double CConfig::GetSurface_Pressure ( unsigned short  val_imarker)
inline

Get the pressure at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The pressure.

Definition at line 192 of file config_structure.inl.

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◆ GetSurface_PressureDrop()

su2double CConfig::GetSurface_PressureDrop ( unsigned short  val_imarker)
inline

Get the pressure drop between two surfaces.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The pressure drop.

Definition at line 212 of file config_structure.inl.

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◆ GetSurface_SecondaryStrength()

su2double CConfig::GetSurface_SecondaryStrength ( unsigned short  val_imarker)
inline

Get the secondary flow strength at the surface.

Parameters
[in]val_imarker- Index corresponding to the outlet boundary.
Returns
The secondary flow strength.

Definition at line 202 of file config_structure.inl.

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◆ GetSurface_SecondOverUniform()

su2double CConfig::GetSurface_SecondOverUniform ( unsigned short  val_imarker)
inline

Get the relative secondary flow strength at the surface.

Parameters
[in]val_imarker- Index corresponding to the outlet boundary.
Returns
The relative seondary flow strength.

Definition at line 204 of file config_structure.inl.

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◆ GetSurface_Temperature()

su2double CConfig::GetSurface_Temperature ( unsigned short  val_imarker)
inline

Get the temperature at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The temperature.

Definition at line 190 of file config_structure.inl.

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◆ GetSurface_TotalPressure()

su2double CConfig::GetSurface_TotalPressure ( unsigned short  val_imarker)
inline

Get the total pressure at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The total pressure.

Definition at line 210 of file config_structure.inl.

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◆ GetSurface_TotalTemperature()

su2double CConfig::GetSurface_TotalTemperature ( unsigned short  val_imarker)
inline

Get the total temperature at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The total temperature.

Definition at line 208 of file config_structure.inl.

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◆ GetSurface_Uniformity()

su2double CConfig::GetSurface_Uniformity ( unsigned short  val_imarker)
inline

Get the streamwise flow uniformity at the surface.

Parameters
[in]val_imarker- Index corresponding to the outlet boundary.
Returns
The streamwise flow uniformity.

Definition at line 200 of file config_structure.inl.

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◆ GetSurfAdjCoeff_FileName()

string CConfig::GetSurfAdjCoeff_FileName ( void  )
inline

Get the name of the file with the surface information for the adjoint problem.

Returns
Name of the file with the surface information for the adjoint problem.

Definition at line 1485 of file config_structure.inl.

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◆ GetSurfFlowCoeff_FileName()

string CConfig::GetSurfFlowCoeff_FileName ( void  )
inline

Get the name of the file with the surface information for the flow problem.

Returns
Name of the file with the surface information for the flow problem.

Definition at line 1483 of file config_structure.inl.

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◆ GetSurfHeat_FileName()

string CConfig::GetSurfHeat_FileName ( void  )
inline

Get the name of the file with the structure variables.

Returns
Name of the file with the structure variables.

Definition at line 1463 of file config_structure.inl.

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◆ GetSurfSens_FileName()

string CConfig::GetSurfSens_FileName ( void  )
inline

Get the name of the file with the surface sensitivity (discrete adjoint).

Returns
Name of the file with the surface sensitivity (discrete adjoint).

Definition at line 1487 of file config_structure.inl.

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◆ GetSurfStructure_FileName()

string CConfig::GetSurfStructure_FileName ( void  )
inline

Get the name of the file with the structure variables.

Returns
Name of the file with the structure variables.

Definition at line 1457 of file config_structure.inl.

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◆ GetSystemMeasurements()

unsigned short CConfig::GetSystemMeasurements ( void  )
inline

Governing equations of the flow (it can be different from the run time equation).

Parameters
[in]val_zone- Zone where the soler is applied.
Returns
Governing equation that we are solving.

Definition at line 852 of file config_structure.inl.

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◆ GetTagFFDBox()

string CConfig::GetTagFFDBox ( unsigned short  val_ffd)
inline

Get the FFD Tag of a particular FFD box.

Parameters
[in]val_ffd- Number of the FFD box that we want to read.
Returns
Name of the FFD box.

Definition at line 773 of file config_structure.inl.

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◆ GetTarget_CL()

su2double CConfig::GetTarget_CL ( void  )
inline

Get the value specified for the target CL.

Returns
Value of the target CL.

Definition at line 1757 of file config_structure.inl.

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◆ GetTemperature_Critical()

su2double CConfig::GetTemperature_Critical ( void  )
inline

Get the value of the critical temperature.

Returns
Critical temperature.

Definition at line 868 of file config_structure.inl.

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◆ GetTemperature_FreeStream()

su2double CConfig::GetTemperature_FreeStream ( void  )
inline

Get the value of the frestream temperature.

Returns
Freestream temperature.

Definition at line 484 of file config_structure.inl.

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◆ GetTemperature_Freestream_Solid()

su2double CConfig::GetTemperature_Freestream_Solid ( void  )
inline

Get the temperature in solids at freestream conditions.

Returns
Freestream temperature (solid).

Definition at line 362 of file config_structure.inl.

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◆ GetTemperature_FreeStreamND()

su2double CConfig::GetTemperature_FreeStreamND ( void  )
inline

Get the value of the non-dimensionalized freestream temperature.

Returns
Non-dimensionalized freestream temperature.

Definition at line 540 of file config_structure.inl.

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◆ GetTemperature_Ref()

su2double CConfig::GetTemperature_Ref ( void  )
inline

Get the value of the reference temperature for non-dimensionalization.

Returns
Reference temperature for non-dimensionalization.

Definition at line 514 of file config_structure.inl.

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◆ GetTemperature_ve_FreeStream()

su2double CConfig::GetTemperature_ve_FreeStream ( void  )
inline

Get the value of the frestream vibrational-electronic temperature.

Returns
Freestream temperature.

Definition at line 502 of file config_structure.inl.

◆ GetThermal_Expansion_Coeff()

su2double CConfig::GetThermal_Expansion_Coeff ( void  )
inline

Get the thermal expansion coefficient.

Returns
Value of the thermal expansion coefficient.

Definition at line 462 of file config_structure.inl.

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◆ GetThermal_Expansion_CoeffND()

su2double CConfig::GetThermal_Expansion_CoeffND ( void  )
inline

Get the non-dim. thermal expansion coefficient.

Returns
Value of the non-dim. thermal expansion coefficient.

Definition at line 464 of file config_structure.inl.

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◆ GetThermalConductivity_Solid()

su2double CConfig::GetThermalConductivity_Solid ( void  )
inline

Get the value of the thermal conductivity for solids.

Returns
Thermal conductivity (solid).

Definition at line 508 of file config_structure.inl.

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◆ GetThermalDiffusivity()

su2double CConfig::GetThermalDiffusivity ( void  )
inline

Get the wave speed.

Returns
Value of the wave speed.

Definition at line 358 of file config_structure.inl.

◆ GetThermalDiffusivity_Solid()

su2double CConfig::GetThermalDiffusivity_Solid ( void  )
inline

Get the value of the thermal diffusivity for solids.

Returns
Thermal conductivity (solid).

Definition at line 360 of file config_structure.inl.

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◆ GetTheta_Interior_Penalty_DGFEM()

su2double CConfig::GetTheta_Interior_Penalty_DGFEM ( void  )
inline

Function to make available the multiplication factor theta of the symmetrizing terms in the DG discretization of the viscous terms.

Returns
The specified factor for the DG discretization.

Definition at line 1921 of file config_structure.inl.

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◆ GetTime_Ref()

su2double CConfig::GetTime_Ref ( void  )
inline

Get the value of the reference time for non-dimensionalization.

Returns
Reference time for non-dimensionalization.

Definition at line 522 of file config_structure.inl.

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◆ GetTimeDOFsADER_DG()

su2double * CConfig::GetTimeDOFsADER_DG ( void  )
inline

Get the location of the time DOFs for ADER-DG on the interval [-1..1].

Returns
The location of the time DOFs used in ADER-DG.

Definition at line 793 of file config_structure.inl.

◆ GetTimeIntegrationADER_DG()

su2double * CConfig::GetTimeIntegrationADER_DG ( void  )
inline

Get the location of the time integration points for ADER-DG on the interval [-1..1].

Returns
The location of the time integration points used in ADER-DG.

Definition at line 797 of file config_structure.inl.

◆ GetTke_FreeStream()

su2double CConfig::GetTke_FreeStream ( void  )
inline

Get the value of the non-dimensionalized freestream viscosity.

Returns
Non-dimensionalized freestream viscosity.

Definition at line 556 of file config_structure.inl.

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◆ GetTke_FreeStreamND()

su2double CConfig::GetTke_FreeStreamND ( void  )
inline

Get the value of the non-dimensionalized freestream viscosity.

Returns
Non-dimensionalized freestream viscosity.

Definition at line 552 of file config_structure.inl.

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◆ GetTotal_DynTime()

su2double CConfig::GetTotal_DynTime ( void  )
inline

If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation.

Returns
Value of the time step in an unsteady simulation (non dimensional).

Definition at line 1817 of file config_structure.inl.

◆ GetTotal_UnstTime()

su2double CConfig::GetTotal_UnstTime ( void  )
inline

If we are performing an unsteady simulation, this is the value of max physical time for which we run the simulation.

Returns
Value of the physical time in an unsteady simulation.

Definition at line 1515 of file config_structure.inl.

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◆ GetTotal_UnstTimeND()

su2double CConfig::GetTotal_UnstTimeND ( void  )
inline

If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation.

Returns
Value of the time step in an unsteady simulation (non dimensional).

Definition at line 1507 of file config_structure.inl.

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◆ GetTotalDV_Penalty()

su2double CConfig::GetTotalDV_Penalty ( void  )
inline

Get the penalty weight value for the objective function.

Returns
Penalty weight value for the reference geometry objective function.

Definition at line 1857 of file config_structure.inl.

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◆ GetTotalPressureIn_BC()

su2double CConfig::GetTotalPressureIn_BC ( )

Get the inlet total pressure imposed as BC for internal flow.

Returns
inlet total pressure

Definition at line 7815 of file config_structure.cpp.

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◆ GetTotalTemperatureIn_BC()

su2double CConfig::GetTotalTemperatureIn_BC ( )

Get the inlet total temperature imposed as BC for internal flow.

Returns
inlet total temperature

Definition at line 7834 of file config_structure.cpp.

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◆ GetTranslation_Rate_X()

su2double CConfig::GetTranslation_Rate_X ( unsigned short  val_iZone)
inline

Get the translational velocity of the mesh in the x-direction.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Translational velocity of the mesh in the x-direction.

Definition at line 924 of file config_structure.inl.

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◆ GetTranslation_Rate_Y()

su2double CConfig::GetTranslation_Rate_Y ( unsigned short  val_iZone)
inline

Get the translational velocity of the mesh in the y-direction.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Translational velocity of the mesh in the y-direction.

Definition at line 926 of file config_structure.inl.

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◆ GetTranslation_Rate_Z()

su2double CConfig::GetTranslation_Rate_Z ( unsigned short  val_iZone)
inline

Get the translational velocity of the mesh in the z-direction.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
Returns
Translational velocity of the mesh in the z-direction.

Definition at line 928 of file config_structure.inl.

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◆ GetTranspiration_Objective()

bool CConfig::GetTranspiration_Objective ( void  )
inline

Provides the transpiration objective information.

Returns
Transpiration objective information, if TRUE then the code will add the jet blowing coefficient to the objective.

Definition at line 741 of file config_structure.inl.

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◆ GetTranspirationFileName()

string CConfig::GetTranspirationFileName ( )
inline

Get the name of file containing all transpirations.

Returns
The transpiration

◆ GetTranspirationParams()

void CConfig::GetTranspirationParams ( string  val_marker,
su2double x0,
su2double x1,
su2double x2,
su2double x3,
su2double y0,
su2double y1,
su2double y2,
su2double y3,
su2double eps0,
su2double eps1,
su2double eps2,
su2double eps3 
)

Get the wall transpiration parameters.

Parameters
[in]val_index- Index corresponding to the transpiration boundary.

Definition at line 7994 of file config_structure.cpp.

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◆ GetTranspTag()

string CConfig::GetTranspTag ( unsigned short  val_dv)
inline

Obtain the marker of a transpiration DV.

Parameters
[in]val_dv- Number of the design variable that we want to read.
Returns
Transpiration boundary identification.

Definition at line 739 of file config_structure.inl.

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◆ GetTurb2LamViscRatio_FreeStream()

su2double CConfig::GetTurb2LamViscRatio_FreeStream ( void  )
inline

Get the value of the turbulent to laminar viscosity ratio.

Returns
Ratio of turbulent to laminar viscosity ratio.

Definition at line 574 of file config_structure.inl.

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◆ GetTurbulenceIntensity_FreeStream()

su2double CConfig::GetTurbulenceIntensity_FreeStream ( void  )
inline

Get the value of the non-dimensionalized freestream turbulence intensity.

Returns
Non-dimensionalized freestream intensity.

Definition at line 572 of file config_structure.inl.

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◆ GetUnst_AdjointIter()

long CConfig::GetUnst_AdjointIter ( void  )
inline

Get the starting direct iteration number for the unsteady adjoint (reverse time integration).

Returns
Starting direct iteration number for the unsteady adjoint.

Definition at line 322 of file config_structure.inl.

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◆ GetUnst_CFL()

su2double CConfig::GetUnst_CFL ( void  )
inline

Get the Courant Friedrich Levi number for unsteady simulations.

Returns
CFL number for unsteady simulations.

Definition at line 761 of file config_structure.inl.

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◆ GetUnst_nIntIter()

unsigned long CConfig::GetUnst_nIntIter ( void  )
inline

Get the number of internal iterations.

Returns
Number of internal iterations.

Definition at line 316 of file config_structure.inl.

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◆ GetUnst_RestartIter()

long CConfig::GetUnst_RestartIter ( void  )
inline

Get the restart iteration number for unsteady simulations.

Returns
Restart iteration number for unsteady simulations.

Definition at line 320 of file config_structure.inl.

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◆ GetUnsteady_FileName()

string CConfig::GetUnsteady_FileName ( string  val_filename,
int  val_iter 
)

Augment the input filename with the iteration number for an unsteady file.

Parameters
[in]val_filename- String value of the base filename.
[in]val_iter- Unsteady iteration number or time instance.
Returns
Name of the file with the iteration number for an unsteady solution file.

Definition at line 7055 of file config_structure.cpp.

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◆ GetUnsteady_Simulation()

unsigned short CConfig::GetUnsteady_Simulation ( void  )
inline

Provides information about the time integration, and change the write in the output files information about the iteration.

Returns
The kind of time integration: Steady state, time stepping method (unsteady) or dual time stepping method (unsteady).

Definition at line 1284 of file config_structure.inl.

◆ GetUpdate_Alpha()

unsigned long CConfig::GetUpdate_Alpha ( void  )
inline

Get the value of iterations to re-evaluate the angle of attack.

Returns
Number of iterations.

Definition at line 1767 of file config_structure.inl.

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◆ GetUpdate_AoA()

bool CConfig::GetUpdate_AoA ( void  )
inline

Get information about whether to update the AoA for fixed lift mode.

Returns
TRUE if we should update the AoA for fixed lift mode; otherwise FALSE.

Definition at line 1771 of file config_structure.inl.

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◆ GetUpdate_BCThrust()

unsigned long CConfig::GetUpdate_BCThrust ( void  )
inline

Get the value of iterations to re-evaluate the angle of attack.

Returns
Number of iterations.

Definition at line 1777 of file config_structure.inl.

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◆ GetUpdate_BCThrust_Bool()

bool CConfig::GetUpdate_BCThrust_Bool ( void  )
inline

Get information about whether to update the AoA for fixed lift mode.

Returns
TRUE if we should update the AoA for fixed lift mode; otherwise FALSE.

Definition at line 1773 of file config_structure.inl.

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◆ GetUse_Lumped_MassMatrix_DGFEM()

bool CConfig::GetUse_Lumped_MassMatrix_DGFEM ( void  )
inline

Function to make available whether or not the lumped mass matrix must be used for steady computations.

Returns
The boolean whether or not to use the lumped mass matrix.

Definition at line 1927 of file config_structure.inl.

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◆ GetVelocity_FreeStream()

su2double * CConfig::GetVelocity_FreeStream ( void  )
inline

Get the vector of the dimensionalized freestream velocity.

Returns
Dimensionalized freestream velocity vector.

Definition at line 546 of file config_structure.inl.

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◆ GetVelocity_FreeStreamND()

su2double * CConfig::GetVelocity_FreeStreamND ( void  )
inline

Get the vector of the non-dimensionalized freestream velocity.

Returns
Non-dimensionalized freestream velocity vector.

Definition at line 544 of file config_structure.inl.

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◆ GetVelocity_Ref()

su2double CConfig::GetVelocity_Ref ( void  )
inline

Get the value of the reference velocity for non-dimensionalization.

Returns
Reference velocity for non-dimensionalization.

Definition at line 518 of file config_structure.inl.

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◆ GetVenkat_LimiterCoeff()

su2double CConfig::GetVenkat_LimiterCoeff ( void  )
inline

Get the value of limiter coefficient.

Returns
Value of the limiter coefficient.

Definition at line 605 of file config_structure.inl.

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◆ GetViscosity_FreeStream()

su2double CConfig::GetViscosity_FreeStream ( void  )
inline

Get the value of the frestream temperature.

Returns
Freestream temperature.

Definition at line 488 of file config_structure.inl.

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◆ GetViscosity_FreeStreamND()

su2double CConfig::GetViscosity_FreeStreamND ( void  )
inline

Get the value of the non-dimensionalized freestream viscosity.

Returns
Non-dimensionalized freestream viscosity.

Definition at line 550 of file config_structure.inl.

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◆ GetViscosity_Ref()

su2double CConfig::GetViscosity_Ref ( void  )
inline

Get the value of the reference viscosity for non-dimensionalization.

Returns
Reference viscosity for non-dimensionalization.

Definition at line 524 of file config_structure.inl.

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◆ GetViscous()

bool CConfig::GetViscous ( void  )
inline

Determines if problem is viscous.

Returns
true if Viscous

Definition at line 292 of file config_structure.inl.

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◆ GetVisualize_CV()

long CConfig::GetVisualize_CV ( void  )
inline

Get the node number of the CV to visualize.

Returns
Node number of the CV to visualize.

Definition at line 1745 of file config_structure.inl.

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◆ GetVisualize_Surface_Def()

bool CConfig::GetVisualize_Surface_Def ( void  )
inline

Creates a teot file to visualize the surface deformation deformation made by the DEF software.

Returns
TRUE if the deformation is going to be plotted; otherwise FALSE.

Definition at line 1054 of file config_structure.inl.

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◆ GetVisualize_Volume_Def()

bool CConfig::GetVisualize_Volume_Def ( void  )
inline

Creates a tecplot file to visualize the volume deformation deformation made by the DEF software.

Returns
TRUE if the deformation is going to be plotted; otherwise FALSE.

Definition at line 1052 of file config_structure.inl.

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◆ GetVolSens_FileName()

string CConfig::GetVolSens_FileName ( void  )
inline

Get the name of the file with the volume sensitivity (discrete adjoint).

Returns
Name of the file with the volume sensitivity (discrete adjoint).

Definition at line 1489 of file config_structure.inl.

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◆ GetWall_Functions()

bool CConfig::GetWall_Functions ( void  )
inline

Get information about whether to use wall functions.

Returns
TRUE if wall functions are on; otherwise FALSE.

Definition at line 1747 of file config_structure.inl.

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◆ GetWall_HeatFlux()

su2double CConfig::GetWall_HeatFlux ( string  val_index)

Get the wall heat flux on a constant heat flux boundary.

Parameters
[in]val_index- Index corresponding to the constant heat flux boundary.
Returns
The heat flux.

Definition at line 7972 of file config_structure.cpp.

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◆ GetWallFunction_DoubleInfo()

su2double * CConfig::GetWallFunction_DoubleInfo ( string  val_marker)

Get the additional double info for the wall function treatment for the given boundary marker.

Parameters
[in]val_marker- String of the viscous wall marker.
Returns
Pointer to the double info for the given marker.

Definition at line 8073 of file config_structure.cpp.

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◆ GetWallFunction_IntInfo()

unsigned short * CConfig::GetWallFunction_IntInfo ( string  val_marker)

Get the additional integer info for the wall function treatment for the given boundary marker.

Parameters
[in]val_marker- String of the viscous wall marker.
Returns
Pointer to the integer info for the given marker.

Definition at line 8060 of file config_structure.cpp.

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◆ GetWallFunction_Treatment()

unsigned short CConfig::GetWallFunction_Treatment ( string  val_marker)

Get the wall function treatment for the given boundary marker.

Parameters
[in]val_marker- String of the viscous wall marker.
Returns
The type of wall function treatment.

Definition at line 8047 of file config_structure.cpp.

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◆ GetWallTemperature()

su2double CConfig::GetWallTemperature ( void  )
inline

Get the value of wall temperature.

Returns
Value of the constant: Temperature

Definition at line 480 of file config_structure.inl.

◆ GetWeakly_Coupled_Heat()

bool CConfig::GetWeakly_Coupled_Heat ( void  )
inline

Get the heat equation.

Returns
YES if weakly coupled heat equation for inc. flow is enabled.

Definition at line 1931 of file config_structure.inl.

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◆ GetWeight_ObjFunc()

su2double CConfig::GetWeight_ObjFunc ( unsigned short  val_obj)
inline

Get the weight of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc.

Author
H. Kline
Note
The objective function will determine the boundary condition of the adjoint problem.
Returns
Weight of objective function.

Definition at line 1276 of file config_structure.inl.

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◆ GetWeightCd()

su2double CConfig::GetWeightCd ( void  )
inline

Value of the weight of the drag coefficient in the Sonic Boom optimization.

Returns
Value of the weight of the drag coefficient in the Sonic Boom optimization.

Definition at line 1543 of file config_structure.inl.

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◆ GetWeightsIntegrationADER_DG()

su2double * CConfig::GetWeightsIntegrationADER_DG ( void  )
inline

Get the weights of the time integration points for ADER-DG.

Returns
The weights of the time integration points used in ADER-DG.

Definition at line 799 of file config_structure.inl.

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◆ GetWind_Gust()

bool CConfig::GetWind_Gust ( void  )
inline

Get information about the wind gust.

Returns
TRUE if there is a wind gust; otherwise FALSE.

Definition at line 1717 of file config_structure.inl.

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◆ GetWrite_Conv_FSI()

bool CConfig::GetWrite_Conv_FSI ( void  )
inline

Write convergence file for FSI problems.

Returns
FALSE means no file is written.

Definition at line 1617 of file config_structure.inl.

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◆ GetWrt_Binary_Restart()

bool CConfig::GetWrt_Binary_Restart ( void  )
inline

Flag for whether binary SU2 native restart files are written.

Returns
Flag for whether binary SU2 native restart files are written, if TRUE then the code will output binary restart files.

Definition at line 1288 of file config_structure.inl.

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◆ GetWrt_Con_Freq()

unsigned long CConfig::GetWrt_Con_Freq ( void  )
inline

Get the frequency for writing the convergence file.

Returns
It writes the convergence file with this frequency.

Definition at line 838 of file config_structure.inl.

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◆ GetWrt_Con_Freq_DualTime()

unsigned long CConfig::GetWrt_Con_Freq_DualTime ( void  )
inline

Get the frequency for writing the convergence file in Dual Time.

Returns
It writes the convergence file with this frequency.

Definition at line 842 of file config_structure.inl.

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◆ GetWrt_Crd_Sol()

bool CConfig::GetWrt_Crd_Sol ( void  )
inline

Get information about writing a binary coordinates file.

Returns
TRUE means that a binary coordinates file will be written.

Definition at line 1657 of file config_structure.inl.

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◆ GetWrt_Csv_Sol()

bool CConfig::GetWrt_Csv_Sol ( void  )
inline

Get information about writing a surface comma-separated values (CSV) solution file.

Returns
TRUE means that a surface comma-separated values (CSV) solution file will be written.

Definition at line 1655 of file config_structure.inl.

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◆ GetWrt_Dynamic()

bool CConfig::GetWrt_Dynamic ( void  )
inline

Get information about writing dynamic structural analysis headers and file extensions.

Returns
TRUE means that dynamic structural analysis solution files will be written.

Definition at line 1825 of file config_structure.inl.

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◆ GetWrt_Halo()

bool CConfig::GetWrt_Halo ( void  )
inline

Get information about writing rind layers to the solution files.

Returns
TRUE means that rind layers will be written to the solution file.

Definition at line 1667 of file config_structure.inl.

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◆ GetWrt_InletFile()

bool CConfig::GetWrt_InletFile ( void  )
inline

Get information about writing a template inlet profile file.

Returns
TRUE means that a template inlet profile file will be written.

Definition at line 1671 of file config_structure.inl.

◆ GetWrt_Limiters()

bool CConfig::GetWrt_Limiters ( void  )
inline

Get information about writing residuals to volume solution file.

Returns
TRUE means that residuals will be written to the solution file.

Definition at line 1661 of file config_structure.inl.

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◆ GetWrt_Output()

bool CConfig::GetWrt_Output ( void  )
inline

Get information about writing output files.

Returns
TRUE means that output files will be written.

Definition at line 1649 of file config_structure.inl.

◆ GetWrt_Performance()

bool CConfig::GetWrt_Performance ( void  )
inline

Get information about writing the performance summary at the end of a calculation.

Returns
TRUE means that the performance summary will be written at the end of a calculation.

Definition at line 1669 of file config_structure.inl.

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◆ GetWrt_Residuals()

bool CConfig::GetWrt_Residuals ( void  )
inline

Get information about writing residuals to volume solution file.

Returns
TRUE means that residuals will be written to the solution file.

Definition at line 1659 of file config_structure.inl.

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◆ GetWrt_SharpEdges()

bool CConfig::GetWrt_SharpEdges ( void  )
inline

Get information about writing residuals to volume solution file.

Returns
TRUE means that residuals will be written to the solution file.

Definition at line 1665 of file config_structure.inl.

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◆ GetWrt_Slice()

bool CConfig::GetWrt_Slice ( void  )
inline

Get information about writing a 1D slice of a 2D cartesian solution.

Returns
TRUE means that a 1D slice of a 2D cartesian solution will be written.

Definition at line 1675 of file config_structure.inl.

◆ GetWrt_Sol_Freq()

unsigned long CConfig::GetWrt_Sol_Freq ( void  )
inline

Get the frequency for writing the solution file.

Returns
It writes the solution file with this frequency.

Definition at line 834 of file config_structure.inl.

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◆ GetWrt_Sol_Freq_DualTime()

unsigned long CConfig::GetWrt_Sol_Freq_DualTime ( void  )
inline

Get the frequency for writing the solution file in Dual Time.

Returns
It writes the solution file with this frequency.

Definition at line 836 of file config_structure.inl.

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◆ GetWrt_Srf_Sol()

bool CConfig::GetWrt_Srf_Sol ( void  )
inline

Get information about writing a surface solution file.

Returns
TRUE means that a surface solution file will be written.

Definition at line 1653 of file config_structure.inl.

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◆ GetWrt_Surf_Freq_DualTime()

unsigned long CConfig::GetWrt_Surf_Freq_DualTime ( void  )
inline

Get the frequency for writing the surface solution file in Dual Time.

Returns
It writes the surface solution file with this frequency.

Definition at line 1951 of file config_structure.inl.

◆ GetWrt_Surface()

bool CConfig::GetWrt_Surface ( void  )
inline

Write solution at each surface.

Returns
TRUE means that the solution at each surface will be written.

Definition at line 1663 of file config_structure.inl.

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◆ GetWrt_Unsteady()

bool CConfig::GetWrt_Unsteady ( void  )
inline

Get information about writing unsteady headers and file extensions.

Returns
TRUE means that unsteady solution files will be written.

Definition at line 844 of file config_structure.inl.

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◆ GetWrt_Vol_Sol()

bool CConfig::GetWrt_Vol_Sol ( void  )
inline

Get information about writing a volume solution file.

Returns
TRUE means that a volume solution file will be written.

Definition at line 1651 of file config_structure.inl.

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◆ Low_Mach_Correction()

bool CConfig::Low_Mach_Correction ( void  )
inline

Get information about the Low Mach Correction.

Returns
TRUE if we are using low Mach correction; otherwise FALSE.

Definition at line 1589 of file config_structure.inl.

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◆ Low_Mach_Preconditioning()

bool CConfig::Low_Mach_Preconditioning ( void  )
inline

Get information about the Low Mach Preconditioning.

Returns
TRUE if we are using low Mach preconditioner; otherwise FALSE.

Definition at line 1587 of file config_structure.inl.

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◆ Set_CrossTerm()

void CConfig::Set_CrossTerm ( bool  needCrossTerm)
inline

Set the boolean addCrossTerm to true or false.

Definition at line 412 of file config_structure.inl.

◆ Set_Electric_Field_Mod()

void CConfig::Set_Electric_Field_Mod ( unsigned short  val_coeff,
su2double  val_el_field 
)
inline

Set the values for the electric field modulus.

Parameters
[in]val_coeff- Index of the electric field.
[in]val_el_field- Value of the electric field.

Definition at line 1841 of file config_structure.inl.

◆ SetActDisk_Area()

void CConfig::SetActDisk_Area ( unsigned short  val_imarker,
su2double  val_actdisk_area 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 162 of file config_structure.inl.

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◆ SetActDisk_BCThrust() [1/2]

void CConfig::SetActDisk_BCThrust ( string  val_marker,
su2double  val_actdisk_bcthrust 
)

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 7487 of file config_structure.cpp.

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◆ SetActDisk_BCThrust() [2/2]

void CConfig::SetActDisk_BCThrust ( unsigned short  val_imarker,
su2double  val_actdisk_bcthrust 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 156 of file config_structure.inl.

◆ SetActDisk_BCThrust_Old() [1/2]

void CConfig::SetActDisk_BCThrust_Old ( string  val_marker,
su2double  val_actdisk_bcthrust_old 
)

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 7495 of file config_structure.cpp.

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◆ SetActDisk_BCThrust_Old() [2/2]

void CConfig::SetActDisk_BCThrust_Old ( unsigned short  val_imarker,
su2double  val_actdisk_bcthrust_old 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 158 of file config_structure.inl.

◆ SetActDisk_DeltaPress()

void CConfig::SetActDisk_DeltaPress ( unsigned short  val_imarker,
su2double  val_actdisk_deltapress 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 98 of file config_structure.inl.

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◆ SetActDisk_DeltaTemp()

void CConfig::SetActDisk_DeltaTemp ( unsigned short  val_imarker,
su2double  val_actdisk_deltatemp 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 144 of file config_structure.inl.

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◆ SetActDisk_Force()

void CConfig::SetActDisk_Force ( unsigned short  val_imarker,
su2double  val_actdisk_force 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 106 of file config_structure.inl.

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◆ SetActDisk_GrossThrust()

void CConfig::SetActDisk_GrossThrust ( unsigned short  val_imarker,
su2double  val_actdisk_grossthrust 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 160 of file config_structure.inl.

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◆ SetActDisk_Mach()

void CConfig::SetActDisk_Mach ( unsigned short  val_imarker,
su2double  val_actdisk_mach 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 104 of file config_structure.inl.

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◆ SetActDisk_MassFlow()

void CConfig::SetActDisk_MassFlow ( unsigned short  val_imarker,
su2double  val_actdisk_massflow 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 102 of file config_structure.inl.

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◆ SetActDisk_NetThrust()

void CConfig::SetActDisk_NetThrust ( unsigned short  val_imarker,
su2double  val_actdisk_netthrust 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 154 of file config_structure.inl.

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◆ SetActDisk_Power()

void CConfig::SetActDisk_Power ( unsigned short  val_imarker,
su2double  val_actdisk_power 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 100 of file config_structure.inl.

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◆ SetActDisk_StaticPressRatio()

void CConfig::SetActDisk_StaticPressRatio ( unsigned short  val_imarker,
su2double  val_actdisk_pressratio 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 150 of file config_structure.inl.

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◆ SetActDisk_StaticTempRatio()

void CConfig::SetActDisk_StaticTempRatio ( unsigned short  val_imarker,
su2double  val_actdisk_tempratio 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 152 of file config_structure.inl.

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◆ SetActDisk_TotalPressRatio()

void CConfig::SetActDisk_TotalPressRatio ( unsigned short  val_imarker,
su2double  val_actdisk_pressratio 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 146 of file config_structure.inl.

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◆ SetActDisk_TotalTempRatio()

void CConfig::SetActDisk_TotalTempRatio ( unsigned short  val_imarker,
su2double  val_actdisk_tempratio 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 148 of file config_structure.inl.

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◆ SetActDiskInlet_Force()

void CConfig::SetActDiskInlet_Force ( unsigned short  val_imarker,
su2double  val_actdisk_force 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 240 of file config_structure.inl.

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◆ SetActDiskInlet_MassFlow()

void CConfig::SetActDiskInlet_MassFlow ( unsigned short  val_imarker,
su2double  val_actdisk_massflow 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 248 of file config_structure.inl.

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◆ SetActDiskInlet_Power()

void CConfig::SetActDiskInlet_Power ( unsigned short  val_imarker,
su2double  val_actdisk_power 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 242 of file config_structure.inl.

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◆ SetActDiskInlet_Pressure()

void CConfig::SetActDiskInlet_Pressure ( unsigned short  val_imarker,
su2double  val_actdisk_pressure 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 234 of file config_structure.inl.

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◆ SetActDiskInlet_RamDrag()

void CConfig::SetActDiskInlet_RamDrag ( unsigned short  val_imarker,
su2double  val_actdisk_ramdrag 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 238 of file config_structure.inl.

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◆ SetActDiskInlet_ReverseMassFlow()

void CConfig::SetActDiskInlet_ReverseMassFlow ( unsigned short  val_imarker,
su2double  val_actdisk_area 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 164 of file config_structure.inl.

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◆ SetActDiskInlet_Temperature()

void CConfig::SetActDiskInlet_Temperature ( unsigned short  val_imarker,
su2double  val_actdisk_temp 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 244 of file config_structure.inl.

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◆ SetActDiskInlet_TotalPressure()

void CConfig::SetActDiskInlet_TotalPressure ( unsigned short  val_imarker,
su2double  val_actdisk_totalpressure 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 236 of file config_structure.inl.

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◆ SetActDiskInlet_TotalTemperature()

void CConfig::SetActDiskInlet_TotalTemperature ( unsigned short  val_imarker,
su2double  val_actdisk_totaltemp 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 246 of file config_structure.inl.

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◆ SetActDiskOutlet_Force()

void CConfig::SetActDiskOutlet_Force ( unsigned short  val_imarker,
su2double  val_actdisk_force 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 256 of file config_structure.inl.

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◆ SetActDiskOutlet_GrossThrust()

void CConfig::SetActDiskOutlet_GrossThrust ( unsigned short  val_imarker,
su2double  val_actdisk_grossthrust 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 254 of file config_structure.inl.

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◆ SetActDiskOutlet_MassFlow()

void CConfig::SetActDiskOutlet_MassFlow ( unsigned short  val_imarker,
su2double  val_actdisk_massflow 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 264 of file config_structure.inl.

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◆ SetActDiskOutlet_Power()

void CConfig::SetActDiskOutlet_Power ( unsigned short  val_imarker,
su2double  val_actdisk_power 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 258 of file config_structure.inl.

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◆ SetActDiskOutlet_Pressure()

void CConfig::SetActDiskOutlet_Pressure ( unsigned short  val_imarker,
su2double  val_actdisk_pressure 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 250 of file config_structure.inl.

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◆ SetActDiskOutlet_Temperature()

void CConfig::SetActDiskOutlet_Temperature ( unsigned short  val_imarker,
su2double  val_actdisk_temp 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 260 of file config_structure.inl.

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◆ SetActDiskOutlet_TotalPressure()

void CConfig::SetActDiskOutlet_TotalPressure ( unsigned short  val_imarker,
su2double  val_actdisk_totalpressure 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 252 of file config_structure.inl.

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◆ SetActDiskOutlet_TotalTemperature()

void CConfig::SetActDiskOutlet_TotalTemperature ( unsigned short  val_imarker,
su2double  val_actdisk_totaltemp 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 262 of file config_structure.inl.

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◆ SetAeroelastic_n()

void CConfig::SetAeroelastic_n ( void  )
inline

Value of Aeroelastic solution coordinate at time n from time n+1.

Definition at line 1699 of file config_structure.inl.

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◆ SetAeroelastic_n1()

void CConfig::SetAeroelastic_n1 ( void  )
inline

Value of Aeroelastic solution coordinate at time n-1 from time n.

Definition at line 1695 of file config_structure.inl.

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◆ SetAeroelastic_np1()

void CConfig::SetAeroelastic_np1 ( unsigned short  iMarker,
vector< vector< su2double > >  solution 
)
inline

Value of Aeroelastic solution coordinate at time n+1.

Definition at line 1685 of file config_structure.inl.

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◆ SetAeroelastic_pitch()

void CConfig::SetAeroelastic_pitch ( unsigned short  val_marker,
su2double  val 
)
inline

Value of pitching coordinate.

Parameters
[in]val_marker- the marker we are monitoring.
[in]val- value of pitching coordinate.

Definition at line 1693 of file config_structure.inl.

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◆ SetAeroelastic_plunge()

void CConfig::SetAeroelastic_plunge ( unsigned short  val_marker,
su2double  val 
)
inline

Value of plunging coordinate.

Parameters
[in]val_marker- the marker we are monitoring.
[in]val- value of plunging coordinate.

Definition at line 1691 of file config_structure.inl.

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◆ SetAoA()

void CConfig::SetAoA ( su2double  val_AoA)
inline

Set the angle of attack.

Parameters
[in]val_AoA- Value of the angle of attack.

Definition at line 709 of file config_structure.inl.

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◆ SetAoA_Offset()

void CConfig::SetAoA_Offset ( su2double  val_AoA_offset)
inline

Set the off set angle of attack.

Parameters
[in]val_AoA- Value of the angle of attack.

Definition at line 711 of file config_structure.inl.

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◆ SetAoA_Sens()

void CConfig::SetAoA_Sens ( su2double  val_AoA_sens)
inline

Set the angle of attack.

Parameters
[in]val_AoA- Value of the angle of attack.

Definition at line 715 of file config_structure.inl.

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◆ SetAoS()

void CConfig::SetAoS ( su2double  val_AoS)
inline

Set the angle of attack.

Parameters
[in]val_AoA- Value of the angle of attack.

Definition at line 717 of file config_structure.inl.

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◆ SetAoS_Offset()

void CConfig::SetAoS_Offset ( su2double  val_AoS_offset)
inline

Set the off set sideslip angle.

Parameters
[in]val_AoA- Value of the off set sideslip angle.

Definition at line 713 of file config_structure.inl.

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◆ SetCFL()

void CConfig::SetCFL ( unsigned short  val_mesh,
su2double  val_cfl 
)
inline

Get the Courant Friedrich Levi number for each grid.

Parameters
[in]val_mesh- Index of the mesh were the CFL is applied.
Returns
CFL number for each grid.

Definition at line 759 of file config_structure.inl.

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◆ SetConductivity_Ref()

void CConfig::SetConductivity_Ref ( su2double  val_conductivity_ref)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 701 of file config_structure.inl.

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◆ SetConfig_Parsing()

void CConfig::SetConfig_Parsing ( char  case_filename[MAX_STRING_SIZE])

Set the config file parsing.

Definition at line 2282 of file config_structure.cpp.

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◆ SetdCD_dCL()

void CConfig::SetdCD_dCL ( su2double  val_dcd_dcl)
inline

Value of the weight of the CD, CL, CM optimization.

Returns
Value of the weight of the CD, CL, CM optimization.

Definition at line 1553 of file config_structure.inl.

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◆ SetdCD_dCMy()

void CConfig::SetdCD_dCMy ( su2double  val_dcd_dcmy)
inline

Value of the weight of the CD, CL, CM optimization.

Returns
Value of the weight of the CD, CL, CM optimization.

Definition at line 1567 of file config_structure.inl.

◆ SetdCL_dAlpha()

void CConfig::SetdCL_dAlpha ( su2double  val_dcl_dalpha)
inline

Value of the weight of the CD, CL, CM optimization.

Returns
Value of the weight of the CD, CL, CM optimization.

Definition at line 1561 of file config_structure.inl.

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◆ SetdCM_diH()

void CConfig::SetdCM_diH ( su2double  val_dcm_dhi)
inline

Value of the weight of the CD, CL, CM optimization.

Returns
Value of the weight of the CD, CL, CM optimization.

Definition at line 1563 of file config_structure.inl.

◆ SetdCMx_dCL()

void CConfig::SetdCMx_dCL ( su2double  val_dcmx_dcl)
inline

Value of the weight of the CD, CL, CM optimization.

Returns
Value of the weight of the CD, CL, CM optimization.

Definition at line 1555 of file config_structure.inl.

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◆ SetdCMy_dCL()

void CConfig::SetdCMy_dCL ( su2double  val_dcmy_dcl)
inline

Value of the weight of the CD, CL, CM optimization.

Returns
Value of the weight of the CD, CL, CM optimization.

Definition at line 1557 of file config_structure.inl.

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◆ SetdCMz_dCL()

void CConfig::SetdCMz_dCL ( su2double  val_dcmz_dcl)
inline

Value of the weight of the CD, CL, CM optimization.

Returns
Value of the weight of the CD, CL, CM optimization.

Definition at line 1559 of file config_structure.inl.

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◆ SetDelta_UnstTimeND()

void CConfig::SetDelta_UnstTimeND ( su2double  val_delta_unsttimend)
inline

Set the value of the unsteadty time step using the CFL number.

Parameters
[in]val_delta_unsttimend- Value of the unsteady time step using CFL number.

Definition at line 1513 of file config_structure.inl.

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◆ SetDensity_FreeStream()

void CConfig::SetDensity_FreeStream ( su2double  val_density_freestream)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 625 of file config_structure.inl.

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◆ SetDensity_FreeStreamND()

void CConfig::SetDensity_FreeStreamND ( su2double  val_density_freestreamnd)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 623 of file config_structure.inl.

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◆ SetDensity_Ref()

void CConfig::SetDensity_Ref ( su2double  val_density_ref)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 677 of file config_structure.inl.

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◆ SetdNetThrust_dBCThrust()

void CConfig::SetdNetThrust_dBCThrust ( su2double  val_dnetthrust_dbcthrust)

Value of the weight of the CD, CL, CM optimization.

Returns
Value of the weight of the CD, CL, CM optimization.

◆ SetDomainVolume()

void CConfig::SetDomainVolume ( su2double  val_volume)
inline

Set the value of the domain volume computed on the finest grid.

Note
This volume do not include the volume of the body that is being simulated.
Parameters
[in]val_volume- Value of the domain volume computed on the finest grid.

Definition at line 430 of file config_structure.inl.

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◆ SetDV_Value()

void CConfig::SetDV_Value ( unsigned short  val_dv,
unsigned short  val_ind,
su2double  val 
)
inline

Set the value of the design variable step, we use this value in design problems.

Parameters
[in]val_dv- Number of the design variable that we want to read.
[in]val- Value of the design variable.

Definition at line 1527 of file config_structure.inl.

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◆ SetEnergy_FreeStream()

void CConfig::SetEnergy_FreeStream ( su2double  val_energy_freestream)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 661 of file config_structure.inl.

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◆ SetEnergy_FreeStreamND()

void CConfig::SetEnergy_FreeStreamND ( su2double  val_energy_freestreamnd)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 659 of file config_structure.inl.

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◆ SetEnergy_Ref()

void CConfig::SetEnergy_Ref ( su2double  val_energy_ref)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 703 of file config_structure.inl.

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◆ SetEngine_Area()

void CConfig::SetEngine_Area ( unsigned short  val_imarker,
su2double  val_engine_area 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_imarker- Index corresponding to a particular engine boundary.
[in]val_engine_area- Exhaust power.

Definition at line 96 of file config_structure.inl.

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◆ SetEngine_Force()

void CConfig::SetEngine_Force ( unsigned short  val_imarker,
su2double  val_engine_force 
)
inline

Set the back pressure (static) at an outlet boundary.

Parameters
[in]val_imarker- Index corresponding to a particular engine boundary.
[in]val_engine_force- Exhaust power.

Definition at line 88 of file config_structure.inl.

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◆ SetEngine_GrossThrust()

void CConfig::SetEngine_GrossThrust ( unsigned short  val_imarker,
su2double  val_engine_grossthrust 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_imarker- Index corresponding to a particular engine boundary.
[in]val_engine_grossthrust- Exhaust power.

Definition at line 94 of file config_structure.inl.

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◆ SetEngine_Mach()

void CConfig::SetEngine_Mach ( unsigned short  val_imarker,
su2double  val_engine_mach 
)
inline

Set the back pressure (static) at an outlet boundary.

Parameters
[in]val_imarker- Index corresponding to a particular engine boundary.
[in]val_engine_mach- Exhaust power.

Definition at line 86 of file config_structure.inl.

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◆ SetEngine_NetThrust()

void CConfig::SetEngine_NetThrust ( unsigned short  val_imarker,
su2double  val_engine_netthrust 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_imarker- Index corresponding to a particular engine boundary.
[in]val_engine_netthrust- Exhaust power.

Definition at line 92 of file config_structure.inl.

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◆ SetEngine_Power()

void CConfig::SetEngine_Power ( unsigned short  val_imarker,
su2double  val_engine_power 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_imarker- Index corresponding to a particular engine boundary.
[in]val_engine_power- Exhaust power.

Definition at line 90 of file config_structure.inl.

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◆ SetEulerPersson()

void CConfig::SetEulerPersson ( bool  val_EulerPersson)
inline

Set boolean for using Persson's shock capturing method in Euler flow DG-FEM.

Parameters
[in]val_EulerPersson- Boolean for using Persson's shock capturing method in Euler flow DG-FEM

Definition at line 1869 of file config_structure.inl.

◆ SetExhaust_Force()

void CConfig::SetExhaust_Force ( unsigned short  val_imarker,
su2double  val_exhaust_force 
)
inline

Set the force balance at an engine exhaust boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
[in]val_exhaust_force- Exhaust force balance.

Definition at line 82 of file config_structure.inl.

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◆ SetExhaust_GrossThrust()

void CConfig::SetExhaust_GrossThrust ( unsigned short  val_imarker,
su2double  val_exhaust_grossthrust 
)
inline

Set the gross thrust at an engine exhaust boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
[in]val_exhaust_grossthrust- Exhaust gross thrust temperature.

Definition at line 80 of file config_structure.inl.

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◆ SetExhaust_MassFlow()

void CConfig::SetExhaust_MassFlow ( unsigned short  val_imarker,
su2double  val_exhaust_massflow 
)
inline

Set the back pressure (static) at an engine exhaust boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
[in]val_exhaust_temp- Exhaust static temperature.

Definition at line 74 of file config_structure.inl.

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◆ SetExhaust_Power()

void CConfig::SetExhaust_Power ( unsigned short  val_imarker,
su2double  val_exhaust_power 
)
inline

Set the power at an engine exhaust boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
[in]val_exhaust_power- Exhaust power.

Definition at line 84 of file config_structure.inl.

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◆ SetExhaust_Pressure()

void CConfig::SetExhaust_Pressure ( unsigned short  val_imarker,
su2double  val_exhaust_pressure 
)
inline

Set the back pressure (static) at an engine exhaust boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
[in]val_exhaust_pressure- Exhaust static pressure.

Definition at line 70 of file config_structure.inl.

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◆ SetExhaust_Temperature()

void CConfig::SetExhaust_Temperature ( unsigned short  val_imarker,
su2double  val_exhaust_temp 
)
inline

Set the temperature (static) at an engine exhaust boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
[in]val_exhaust_temp- Exhaust static temperature.

Definition at line 72 of file config_structure.inl.

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◆ SetExhaust_TotalPressure()

void CConfig::SetExhaust_TotalPressure ( unsigned short  val_imarker,
su2double  val_exhaust_totalpressure 
)
inline

Set the back pressure (total) at an engine exhaust boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
[in]val_exhaust_totalpressure- Exhaust total pressure.

Definition at line 76 of file config_structure.inl.

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◆ SetExhaust_TotalTemperature()

void CConfig::SetExhaust_TotalTemperature ( unsigned short  val_imarker,
su2double  val_exhaust_totaltemp 
)
inline

Set the total temperature at an engine exhaust boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
[in]val_exhaust_totaltemp- Exhaust total temperature.

Definition at line 78 of file config_structure.inl.

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◆ SetExtIter()

void CConfig::SetExtIter ( unsigned long  val_iter)
inline

Set the current external iteration number.

Parameters
[in]val_iter- Current external iteration number.

Definition at line 300 of file config_structure.inl.

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◆ SetExtIter_OffSet()

void CConfig::SetExtIter_OffSet ( unsigned long  val_iter)
inline

Set the current external iteration number.

Parameters
[in]val_iter- Current external iteration number.

Definition at line 302 of file config_structure.inl.

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◆ SetFinestMesh()

void CConfig::SetFinestMesh ( unsigned short  val_finestmesh)
inline

Set the finest mesh in a multigrid strategy.

Note
If we are using a Full Multigrid Strategy or a start up with finest grid, it is necessary to change several times the finest grid.
Parameters
[in]val_finestmesh- Index of the finest grid.

Definition at line 733 of file config_structure.inl.

◆ SetForce_Ref()

void CConfig::SetForce_Ref ( su2double  val_force_ref)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 685 of file config_structure.inl.

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◆ SetFreeStreamTurboNormal()

void CConfig::SetFreeStreamTurboNormal ( su2double turboNormal)

Set freestream turbonormal for initializing solution.

Definition at line 8908 of file config_structure.cpp.

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◆ SetFroude()

void CConfig::SetFroude ( su2double  val_froude)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 665 of file config_structure.inl.

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◆ SetFSIIter()

void CConfig::SetFSIIter ( unsigned long  val_iter)
inline

Set the current FSI iteration number.

Parameters
[in]val_iter- Current FSI iteration number.

Definition at line 304 of file config_structure.inl.

◆ SetGas_Constant()

void CConfig::SetGas_Constant ( su2double  val_gas_constant)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 689 of file config_structure.inl.

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◆ SetGas_Constant_Ref()

void CConfig::SetGas_Constant_Ref ( su2double  val_gas_constant_ref)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 687 of file config_structure.inl.

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◆ SetGas_ConstantND()

void CConfig::SetGas_ConstantND ( su2double  val_gas_constantnd)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 637 of file config_structure.inl.

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◆ SetGiles_Var1()

void CConfig::SetGiles_Var1 ( su2double  newVar1,
string  val_marker 
)

Set the var 1 for Giles BC.

Parameters
[in]val_marker- Index corresponding to the Giles BC.

Definition at line 7741 of file config_structure.cpp.

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◆ SetGlobalParam()

void CConfig::SetGlobalParam ( unsigned short  val_solver,
unsigned short  val_system,
unsigned long  val_extiter 
)

Set the global parameters of each simulation for each runtime system.

Parameters
[in]val_solver- Solver of the simulation.
[in]val_system- Runtime system that we are solving.

Definition at line 7239 of file config_structure.cpp.

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◆ SetHeat_Flux_Ref()

void CConfig::SetHeat_Flux_Ref ( su2double  val_heat_flux_ref)
inline

Set the heat flux reference value.

Returns
Value of the reference heat flux.

Definition at line 697 of file config_structure.inl.

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◆ SetHistFile()

void CConfig::SetHistFile ( ofstream *  HistFile)
inline

Set the ofstream of the history file for the current zone.

Definition at line 1965 of file config_structure.inl.

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◆ SetiInst()

void CConfig::SetiInst ( unsigned short  val_iInst)
inline

Set the current instance.

Parameters
[in]iInst- current instance identifier.

Definition at line 1823 of file config_structure.inl.

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◆ SetIncInlet_BC()

void CConfig::SetIncInlet_BC ( su2double  val_in)

Set the inlet velocity or pressure imposed as BC for incompressible flow.

Parameters
[in]val_in- New value of the inlet velocity or pressure.

Definition at line 7907 of file config_structure.cpp.

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◆ SetIncPressureOut_BC()

void CConfig::SetIncPressureOut_BC ( su2double  val_pressure)

Set the outlet pressure imposed as BC for incompressible flow.

Parameters
[in]val_pressure- New value of the outlet pressure.

Definition at line 7950 of file config_structure.cpp.

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◆ SetIncTemperature_BC()

void CConfig::SetIncTemperature_BC ( su2double  val_temperature)

Set the inlet temperature imposed as BC for incompressible flow.

Parameters
[in]val_temperature- New value of the inlet temperature.

Definition at line 7929 of file config_structure.cpp.

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◆ SetInflow_Force()

void CConfig::SetInflow_Force ( unsigned short  val_imarker,
su2double  val_fanface_force 
)
inline

Set the force balance at an engine inflow boundary.

Parameters
[in]val_index- Index corresponding to the engine inflow boundary.
[in]val_fanface_force- Fan face force.

Definition at line 64 of file config_structure.inl.

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◆ SetInflow_Mach()

void CConfig::SetInflow_Mach ( unsigned short  val_imarker,
su2double  val_fanface_mach 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 48 of file config_structure.inl.

◆ SetInflow_MassFlow()

void CConfig::SetInflow_MassFlow ( unsigned short  val_imarker,
su2double  val_fanface_massflow 
)
inline

Set the massflow at an engine inflow boundary.

Parameters
[in]val_index- Index corresponding to the engine inflow boundary.
[in]val_fanface_massflow- Massflow.

Definition at line 52 of file config_structure.inl.

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◆ SetInflow_Power()

void CConfig::SetInflow_Power ( unsigned short  val_imarker,
su2double  val_fanface_power 
)
inline

Set the power at an engine inflow boundary.

Parameters
[in]val_index- Index corresponding to the engine inflow boundary.
[in]val_fanface_force- Power.

Definition at line 66 of file config_structure.inl.

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◆ SetInflow_Pressure()

void CConfig::SetInflow_Pressure ( unsigned short  val_imarker,
su2double  val_fanface_pressure 
)
inline

Set the fan face static pressure at an engine inflow boundary.

Parameters
[in]val_index- Index corresponding to the engine inflow boundary.
[in]val_fanface_pressure- Fan face static pressure.

Definition at line 50 of file config_structure.inl.

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◆ SetInflow_RamDrag()

void CConfig::SetInflow_RamDrag ( unsigned short  val_imarker,
su2double  val_fanface_ramdrag 
)
inline

Set the ram drag temperature at an engine inflow boundary.

Parameters
[in]val_index- Index corresponding to the engine inflow boundary.
[in]val_fanface_ramdrag- Ram drag value.

Definition at line 62 of file config_structure.inl.

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◆ SetInflow_ReverseMassFlow()

void CConfig::SetInflow_ReverseMassFlow ( unsigned short  val_imarker,
su2double  val_fanface_reversemassflow 
)
inline

Set the reverse flow at an engine inflow boundary.

Parameters
[in]val_index- Index corresponding to the engine inflow boundary.
[in]val_fanface_reversemassflow- reverse flow.

Definition at line 54 of file config_structure.inl.

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◆ SetInflow_Temperature()

void CConfig::SetInflow_Temperature ( unsigned short  val_imarker,
su2double  val_fanface_temperature 
)
inline

Set the fan face static temperature at an engine inflow boundary.

Parameters
[in]val_index- Index corresponding to the engine inflow boundary.
[in]val_fanface_pressure- Fan face static temperature.

Definition at line 58 of file config_structure.inl.

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◆ SetInflow_TotalPressure()

void CConfig::SetInflow_TotalPressure ( unsigned short  val_imarker,
su2double  val_fanface_totalpressure 
)
inline

Set the fan face total pressure at an engine inflow boundary.

Parameters
[in]val_index- Index corresponding to the engine inflow boundary.
[in]val_fanface_totalpressure- Fan face total pressure.

Definition at line 56 of file config_structure.inl.

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◆ SetInflow_TotalTemperature()

void CConfig::SetInflow_TotalTemperature ( unsigned short  val_imarker,
su2double  val_fanface_totaltemperature 
)
inline

Set the fan face total temperature at an engine inflow boundary.

Parameters
[in]val_index- Index corresponding to the engine inflow boundary.
[in]val_fanface_totaltemperature- Fan face total temperature.

Definition at line 60 of file config_structure.inl.

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◆ SetInitial_BCThrust()

void CConfig::SetInitial_BCThrust ( su2double  val_bcthrust)
inline

Get the value of the non-dimensionalized actuator disk turbulence intensity.

Returns
Non-dimensionalized actuator disk intensity.

Definition at line 568 of file config_structure.inl.

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◆ SetInlet_Ptotal()

void CConfig::SetInlet_Ptotal ( su2double  val_pressure,
string  val_marker 
)

Set the total pressure at an inlet boundary.

Parameters
[in]val_pressure- Pressure value at the inlet boundary.
[in]val_index- Index corresponding to the inlet boundary.

Definition at line 7656 of file config_structure.cpp.

◆ SetIntIter()

void CConfig::SetIntIter ( unsigned long  val_iter)
inline

Set the current internal iteration number.

Parameters
[in]val_iter- Current external iteration number.

Definition at line 306 of file config_structure.inl.

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◆ SetKind_AdjTurb_Linear_Prec()

void CConfig::SetKind_AdjTurb_Linear_Prec ( unsigned short  val_kind_prec)
inline

Set the kind of preconditioner for the implicit solver.

Returns
Numerical preconditioner for implicit formulation (solving the linear system).

Definition at line 1024 of file config_structure.inl.

◆ SetKind_AverageProcess()

void CConfig::SetKind_AverageProcess ( unsigned short  new_AverageProcess)
inline

Set the kind of mixing process for averaging quantities at the boundaries.

Returns
Kind of mixing process.

Definition at line 1186 of file config_structure.inl.

◆ SetKind_ConvNumScheme()

void CConfig::SetKind_ConvNumScheme ( unsigned short  val_kind_convnumscheme,
unsigned short  val_kind_centered,
unsigned short  val_kind_upwind,
unsigned short  val_kind_slopelimit,
bool  val_muscl,
unsigned short  val_kind_fem 
)

Set the parameters of the convective numerical scheme.

Note
The parameters will change because we are solving different kind of equations.
Parameters
[in]val_kind_convnumscheme- Center or upwind scheme.
[in]val_kind_centered- If centered scheme, kind of centered scheme (JST, etc.).
[in]val_kind_upwind- If upwind scheme, kind of upwind scheme (Roe, etc.).
[in]val_kind_slopelimit- If upwind scheme, kind of slope limit.
[in]val_muscl- Define if we apply a MUSCL scheme or not.
[in]val_kind_fem- If FEM, what kind of FEM discretization.

Definition at line 7225 of file config_structure.cpp.

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◆ SetKind_Deform_Linear_Solver_Prec()

void CConfig::SetKind_Deform_Linear_Solver_Prec ( unsigned short  val_kind_prec)
inline

Set the kind of preconditioner for the implicit solver.

Returns
Numerical preconditioner for implicit formulation (solving the linear system).

Definition at line 984 of file config_structure.inl.

◆ SetKind_GridMovement()

void CConfig::SetKind_GridMovement ( unsigned short  val_iZone,
unsigned short  motion_Type 
)
inline

Set the type of dynamic mesh motion.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
[in]motion_Type- Specify motion type.

Definition at line 908 of file config_structure.inl.

◆ SetKind_Linear_Solver_Prec()

void CConfig::SetKind_Linear_Solver_Prec ( unsigned short  val_kind_prec)
inline

Set the kind of preconditioner for the implicit solver.

Returns
Numerical preconditioner for implicit formulation (solving the linear system).

Definition at line 988 of file config_structure.inl.

◆ SetKind_PerformanceAverageProcess()

void CConfig::SetKind_PerformanceAverageProcess ( unsigned short  new_AverageProcess)
inline

Set the kind of mixing process for averaging quantities at the boundaries.

Returns
Kind of mixing process.

Definition at line 1188 of file config_structure.inl.

◆ SetKind_Solver()

void CConfig::SetKind_Solver ( unsigned short  val_solver)
inline

Governing equations of the flow (it can be different from the run time equation).

Parameters
[in]val_zone- Zone where the soler is applied.
Returns
Governing equation that we are solving.

Definition at line 848 of file config_structure.inl.

◆ SetKind_SU2()

void CConfig::SetKind_SU2 ( unsigned short  val_kind_su2)
inline

Get the kind of SU2 software component.

Returns
Kind of the SU2 software component.

Definition at line 288 of file config_structure.inl.

◆ SetKind_TimeIntScheme()

void CConfig::SetKind_TimeIntScheme ( unsigned short  val_kind_timeintscheme)
inline

Set the kind of time integration scheme.

Note
If we are solving different equations it will be necessary to change several times the kind of time integration, to choose the right scheme.
Parameters
[in]val_kind_timeintscheme- Kind of time integration scheme.

Definition at line 1270 of file config_structure.inl.

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◆ SetKt_ConstantND()

void CConfig::SetKt_ConstantND ( su2double  kt_const)
inline

Set the value of the non-dimensional thermal conductivity.

Definition at line 904 of file config_structure.inl.

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◆ SetLength_Ref()

void CConfig::SetLength_Ref ( su2double  val_length_ref)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 671 of file config_structure.inl.

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◆ SetMach()

void CConfig::SetMach ( su2double  val_mach)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 669 of file config_structure.inl.

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◆ SetMarker_All_Analyze()

void CConfig::SetMarker_All_Analyze ( unsigned short  val_marker,
unsigned short  val_analyze 
)
inline

Set if a marker val_marker is going to be plot val_plotting (read from the config file).

Parameters
[in]val_marker- Index of the marker in which we are interested.
[in]val_plotting- 0 or 1 depending if the the marker is going to be plot.

Definition at line 1343 of file config_structure.inl.

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◆ SetMarker_All_Designing()

void CConfig::SetMarker_All_Designing ( unsigned short  val_marker,
unsigned short  val_designing 
)
inline

Set if a marker val_marker is going to be designed val_designing (read from the config file).

Note
This is important for non dimensional coefficient computation.
Parameters
[in]val_marker- Index of the marker in which we are interested.
[in]val_monitoring- 0 or 1 depending if the the marker is going to be designed.

Definition at line 1339 of file config_structure.inl.

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◆ SetMarker_All_DV()

void CConfig::SetMarker_All_DV ( unsigned short  val_marker,
unsigned short  val_DV 
)
inline

Set if a marker val_marker is going to be affected by design variables val_moving (read from the config file).

Parameters
[in]val_marker- Index of the marker in which we are interested.
[in]val_DV- 0 or 1 depending if the the marker is affected by design variables.

Definition at line 1353 of file config_structure.inl.

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◆ SetMarker_All_GeoEval()

void CConfig::SetMarker_All_GeoEval ( unsigned short  val_marker,
unsigned short  val_geoeval 
)
inline

Set if a marker val_marker is going to be monitored val_monitoring (read from the config file).

Note
This is important for non dimensional coefficient computation.
Parameters
[in]val_marker- Index of the marker in which we are interested.
[in]val_monitoring- 0 or 1 depending if the the marker is going to be monitored.

Definition at line 1337 of file config_structure.inl.

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◆ SetMarker_All_KindBC()

void CConfig::SetMarker_All_KindBC ( unsigned short  val_marker,
unsigned short  val_boundary 
)
inline

Set the value of the boundary val_boundary (read from the config file) for the marker val_marker.

Parameters
[in]val_marker- Index of the marker in which we are interested.
[in]val_boundary- Kind of boundary read from config file.

Definition at line 1331 of file config_structure.inl.

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◆ SetMarker_All_MixingPlaneInterface()

void CConfig::SetMarker_All_MixingPlaneInterface ( unsigned short  val_marker,
unsigned short  val_mixplan_interface 
)
inline

Set if a marker val_marker is part of the MixingPlane interface (read from the config file).

Parameters
[in]val_marker- Index of the marker in which we are interested.
[in]val_turboperf- 0 if not part of the MixingPlane interface or greater than 1 if it is part.

Definition at line 1351 of file config_structure.inl.

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◆ SetMarker_All_Monitoring()

void CConfig::SetMarker_All_Monitoring ( unsigned short  val_marker,
unsigned short  val_monitoring 
)
inline

Set if a marker val_marker is going to be monitored val_monitoring (read from the config file).

Note
This is important for non dimensional coefficient computation.
Parameters
[in]val_marker- Index of the marker in which we are interested.
[in]val_monitoring- 0 or 1 depending if the the marker is going to be monitored.

Definition at line 1335 of file config_structure.inl.

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◆ SetMarker_All_Moving()

void CConfig::SetMarker_All_Moving ( unsigned short  val_marker,
unsigned short  val_moving 
)
inline

Set if a marker val_marker is going to be moved val_moving (read from the config file).

Parameters
[in]val_marker- Index of the marker in which we are interested.
[in]val_moving- 0 or 1 depending if the the marker is going to be moved.

Definition at line 1355 of file config_structure.inl.

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◆ SetMarker_All_PerBound()

void CConfig::SetMarker_All_PerBound ( unsigned short  val_marker,
short  val_perbound 
)
inline

Set if a marker val_marker is going to be periodic val_perbound (read from the config file).

Parameters
[in]val_marker- Index of the marker in which we are interested.
[in]val_perbound- Index of the surface with the periodic boundary.

Definition at line 1359 of file config_structure.inl.

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◆ SetMarker_All_Plotting()

void CConfig::SetMarker_All_Plotting ( unsigned short  val_marker,
unsigned short  val_plotting 
)
inline

Set if a marker val_marker is going to be plot val_plotting (read from the config file).

Parameters
[in]val_marker- Index of the marker in which we are interested.
[in]val_plotting- 0 or 1 depending if the the marker is going to be plot.

Definition at line 1341 of file config_structure.inl.

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◆ SetMarker_All_PyCustom()

void CConfig::SetMarker_All_PyCustom ( unsigned short  val_marker,
unsigned short  val_PyCustom 
)
inline

Set if a marker val_marker is going to be customized in Python val_PyCustom (read from the config file).

Parameters
[in]val_marker- Index of the marker in which we are interested.
[in]val_PyCustom- 0 or 1 depending if the the marker is going to be customized in Python.

Definition at line 1357 of file config_structure.inl.

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◆ SetMarker_All_SendRecv()

void CConfig::SetMarker_All_SendRecv ( unsigned short  val_marker,
short  val_index 
)
inline

Set if a marker val_marker is going to be sent or receive val_index from another domain.

Parameters
[in]val_marker- 0 or 1 depending if the the marker is going to be moved.
[in]val_index- Index of the surface read from geometry file.

Definition at line 1371 of file config_structure.inl.

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◆ SetMarker_All_TagBound()

void CConfig::SetMarker_All_TagBound ( unsigned short  val_marker,
string  val_index 
)
inline

Set the value of the index val_index (read from the geometry file) for the marker val_marker.

Parameters
[in]val_marker- Index of the marker in which we are interested.
[in]val_index- Index of the surface read from geometry file.

Definition at line 1333 of file config_structure.inl.

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◆ SetMarker_All_Turbomachinery()

void CConfig::SetMarker_All_Turbomachinery ( unsigned short  val_marker,
unsigned short  val_turbo 
)
inline

Set if a marker val_marker is part of the Turbomachinery (read from the config file).

Parameters
[in]val_marker- Index of the marker in which we are interested.
[in]val_turboperf- 0 if not part of Turbomachinery or greater than 1 if it is part.

Definition at line 1347 of file config_structure.inl.

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◆ SetMarker_All_TurbomachineryFlag()

void CConfig::SetMarker_All_TurbomachineryFlag ( unsigned short  val_marker,
unsigned short  val_turboflag 
)
inline

Set a flag to the marker val_marker part of the Turbomachinery (read from the config file).

Parameters
[in]val_marker- Index of the marker in which we are interested.
[in]val_turboperflag- 0 if is not part of the Turbomachinery, flag INFLOW or OUTFLOW if it is part.

Definition at line 1349 of file config_structure.inl.

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◆ SetMarker_All_ZoneInterface()

void CConfig::SetMarker_All_ZoneInterface ( unsigned short  val_marker,
unsigned short  val_fsiinterface 
)
inline

Set if a marker val_marker is part of the FSI interface val_plotting (read from the config file).

Parameters
[in]val_marker- Index of the marker in which we are interested.
[in]val_plotting- 0 or 1 depending if the the marker is part of the FSI interface.

Definition at line 1345 of file config_structure.inl.

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◆ SetMarkers()

void CConfig::SetMarkers ( unsigned short  val_software)

Config file markers processing.

Definition at line 4059 of file config_structure.cpp.

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◆ SetMax_Vel2()

void CConfig::SetMax_Vel2 ( su2double  val_max_vel2)
inline

Set the maximum velocity^2 in the domain for the incompressible preconditioner.

Parameters
[in]Valueof the maximum velocity^2 in the domain for the incompressible preconditioner.

Definition at line 1943 of file config_structure.inl.

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◆ SetMGLevels()

void CConfig::SetMGLevels ( unsigned short  val_nMGLevels)
inline

Set the number of multigrid levels.

Parameters
[in]val_nMGLevels- Index of the mesh were the CFL is applied

Definition at line 729 of file config_structure.inl.

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◆ SetModVel_FreeStream()

void CConfig::SetModVel_FreeStream ( su2double  val_modvel_freestream)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 629 of file config_structure.inl.

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◆ SetModVel_FreeStreamND()

void CConfig::SetModVel_FreeStreamND ( su2double  val_modvel_freestreamnd)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 631 of file config_structure.inl.

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◆ SetMonitotOutletPressure()

void CConfig::SetMonitotOutletPressure ( su2double  newMonPres)
inline

Set Monitor Outlet Pressure value for the ramp.

Definition at line 1200 of file config_structure.inl.

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◆ SetMotion_Origin_X()

void CConfig::SetMotion_Origin_X ( unsigned short  val_iZone,
su2double  val_origin 
)
inline

Set x-coordinate of the mesh motion origin.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
[in]val_origin- New x-coordinate of the mesh motion origin.

Definition at line 918 of file config_structure.inl.

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◆ SetMotion_Origin_Y()

void CConfig::SetMotion_Origin_Y ( unsigned short  val_iZone,
su2double  val_origin 
)
inline

Set y-coordinate of the mesh motion origin.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
[in]val_origin- New y-coordinate of the mesh motion origin.

Definition at line 920 of file config_structure.inl.

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◆ SetMotion_Origin_Z()

void CConfig::SetMotion_Origin_Z ( unsigned short  val_iZone,
su2double  val_origin 
)
inline

Set z-coordinate of the mesh motion origin.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
[in]val_origin- New y-coordinate of the mesh motion origin.

Definition at line 922 of file config_structure.inl.

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◆ SetMPICommunicator()

void CConfig::SetMPICommunicator ( SU2_MPI::Comm  Communicator)

Set the MPI communicator for SU2.

Parameters
[in]Communicator- MPI communicator for SU2.

Definition at line 158 of file config_structure.cpp.

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◆ SetMu_ConstantND()

void CConfig::SetMu_ConstantND ( su2double  mu_const)
inline

Set the value of the non-dimensional constant viscosity.

Definition at line 896 of file config_structure.inl.

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◆ SetMu_RefND()

void CConfig::SetMu_RefND ( su2double  mu_ref)
inline

Set the value of the non-dimensional reference viscosity for Sutherland model.

Definition at line 898 of file config_structure.inl.

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◆ SetMu_SND()

void CConfig::SetMu_SND ( su2double  mu_s)
inline

Set the value of the non-dimensional S for Sutherland model.

Definition at line 902 of file config_structure.inl.

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◆ SetMu_Temperature_RefND()

void CConfig::SetMu_Temperature_RefND ( su2double  mu_Tref)
inline

Set the value of the non-dimensional reference temperature for Sutherland model.

Definition at line 900 of file config_structure.inl.

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◆ SetnBlades()

void CConfig::SetnBlades ( unsigned short  val_iZone,
su2double  nblades 
)
inline

number Turbomachinery blades computed using the pitch information.

Returns
nBlades.

Definition at line 1228 of file config_structure.inl.

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◆ SetnExtIter()

void CConfig::SetnExtIter ( unsigned long  val_niter)
inline

Set the number of external iterations.

Note
This is important in no time depending methods, where only one external iteration is needed.
Parameters
[in]val_niter- Set the number of external iterations.

Definition at line 432 of file config_structure.inl.

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◆ SetnLevels_TimeAccurateLTS()

void CConfig::SetnLevels_TimeAccurateLTS ( unsigned short  val_nLevels)
inline

Set the number of time levels for time accurate local time stepping.

Parameters
[in]val_nLevels- The number of time levels to be set.

Definition at line 789 of file config_structure.inl.

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◆ SetnMarker_All()

void CConfig::SetnMarker_All ( unsigned short  val_nmarker)
inline

Stores the number of marker in the simulation.

Parameters
[in]val_nmarker- Number of markers of the problem.

Definition at line 1300 of file config_structure.inl.

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◆ SetNonphysical_Points()

void CConfig::SetNonphysical_Points ( unsigned long  val_nonphys_points)
inline

Set the current number of non-physical nodes in the solution.

Parameters
[in]val_nonphys_points- current number of non-physical points.

Definition at line 1783 of file config_structure.inl.

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◆ SetNonphysical_Reconstr()

void CConfig::SetNonphysical_Reconstr ( unsigned long  val_nonphys_reconstr)
inline

Set the current number of non-physical reconstructions for 2nd-order upwinding.

Parameters
[in]val_nonphys_reconstr- current number of non-physical reconstructions for 2nd-order upwinding.

Definition at line 1787 of file config_structure.inl.

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◆ SetnPeriodicIndex()

void CConfig::SetnPeriodicIndex ( unsigned short  val_index)

Set the total number of SEND_RECEIVE periodic transformations.

Parameters
[in]val_index- Total number of transformations.

Definition at line 7575 of file config_structure.cpp.

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◆ SetnSpan_iZones()

void CConfig::SetnSpan_iZones ( unsigned short  nSpan,
unsigned short  iZone 
)
inline

set number span-wise sections to compute 3D BC and performance for turbomachinery.

Definition at line 1254 of file config_structure.inl.

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◆ SetnSpanMaxAllZones()

void CConfig::SetnSpanMaxAllZones ( unsigned short  val_nSpna_max)
inline

set number of maximum span-wise sections among all zones .

Definition at line 1250 of file config_structure.inl.

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◆ SetnSpanWiseSections()

void CConfig::SetnSpanWiseSections ( unsigned short  nSpan)
inline

set number span-wise sections to compute 3D BC and performance for turbomachinery.

Definition at line 1248 of file config_structure.inl.

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◆ SetOmega_FreeStream()

void CConfig::SetOmega_FreeStream ( su2double  val_omega_freestream)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 657 of file config_structure.inl.

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◆ SetOmega_FreeStreamND()

void CConfig::SetOmega_FreeStreamND ( su2double  val_omega_freestreamnd)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 653 of file config_structure.inl.

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◆ SetOmega_Ref()

void CConfig::SetOmega_Ref ( su2double  val_omega_ref)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 683 of file config_structure.inl.

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◆ SetOpt_RelaxFactor()

void CConfig::SetOpt_RelaxFactor ( su2double  val_scale)
inline

Set the scale factor for the line search.

Parameters
[in]val_scale- scale of the deformation.

Definition at line 1743 of file config_structure.inl.

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◆ SetOutlet_Pressure()

void CConfig::SetOutlet_Pressure ( su2double  val_pressure,
string  val_marker 
)

Set the back pressure (static) at an outlet boundary.

Parameters
[in]val_pressure- Pressure value at the outlet boundary.
[in]val_index- Index corresponding to the outlet boundary.

Definition at line 7698 of file config_structure.cpp.

◆ SetOutput()

void CConfig::SetOutput ( unsigned short  val_software,
unsigned short  val_izone 
)

Config file output.

Definition at line 4658 of file config_structure.cpp.

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◆ SetPeriodicCenter()

void CConfig::SetPeriodicCenter ( unsigned short  val_index,
su2double center 
)
inline

Set the rotation center for a periodic transformation.

Parameters
[in]val_index- Index corresponding to the periodic transformation.
[in]center- Pointer to a vector containing the coordinate of the center.

Definition at line 1625 of file config_structure.inl.

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◆ SetPeriodicRotation()

void CConfig::SetPeriodicRotation ( unsigned short  val_index,
su2double rotation 
)
inline

Set the rotation angles for a periodic transformation.

Parameters
[in]val_index- Index corresponding to the periodic transformation.
[in]rotation- Pointer to a vector containing the rotation angles.

Definition at line 1631 of file config_structure.inl.

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◆ SetPeriodicTranslate()

void CConfig::SetPeriodicTranslate ( unsigned short  val_index,
su2double translate 
)
inline

Set the translation vector for a periodic transformation.

Parameters
[in]val_index- Index corresponding to the periodic transformation.
[in]translate- Pointer to a vector containing the coordinate of the center.

Definition at line 1637 of file config_structure.inl.

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◆ SetPointersNull()

void CConfig::SetPointersNull ( void  )

Initializes pointers to null.

Definition at line 359 of file config_structure.cpp.

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◆ SetPostprocessing()

void CConfig::SetPostprocessing ( unsigned short  val_software,
unsigned short  val_izone,
unsigned short  val_nDim 
)

Config file postprocessing.

Definition at line 2467 of file config_structure.cpp.

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◆ SetPressure_FreeStream()

void CConfig::SetPressure_FreeStream ( su2double  val_pressure_freestream)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 617 of file config_structure.inl.

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◆ SetPressure_FreeStreamND()

void CConfig::SetPressure_FreeStreamND ( su2double  val_pressure_freestreamnd)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 615 of file config_structure.inl.

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◆ SetPressure_Ref()

void CConfig::SetPressure_Ref ( su2double  val_pressure_ref)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 675 of file config_structure.inl.

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◆ SetPressure_Thermodynamic()

void CConfig::SetPressure_Thermodynamic ( su2double  val_pressure_thermodynamic)
inline

Set the thermodynamic pressure for low Mach problems.

Returns
Value of the thermodynamic pressure.

Definition at line 621 of file config_structure.inl.

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◆ SetPressure_ThermodynamicND()

void CConfig::SetPressure_ThermodynamicND ( su2double  val_pressure_thermodynamicnd)
inline

Set the non-dimensionalized thermodynamic pressure for low Mach problems.

Returns
Value of the non-dimensionalized thermodynamic pressure.

Definition at line 619 of file config_structure.inl.

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◆ SetPressureOut_BC()

void CConfig::SetPressureOut_BC ( su2double  val_press)

Set the outlet pressure imposed as BC for internal flow.

Parameters
[in]val_temp- New value of the outlet pressure.

Definition at line 7801 of file config_structure.cpp.

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◆ SetProfilingCSV()

void CConfig::SetProfilingCSV ( void  )

Write a CSV file containing the results of the profiling.

Definition at line 8514 of file config_structure.cpp.

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◆ SetRefArea()

void CConfig::SetRefArea ( su2double  val_area)
inline

In case the RefArea is equal to 0 then, it is necessary to compute a reference area, with this function we set the value of the reference area.

Parameters
[in]val_area- Value of the reference area for non dimensional coefficient computation.

Definition at line 426 of file config_structure.inl.

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◆ SetRefOriginMoment_X()

void CConfig::SetRefOriginMoment_X ( unsigned short  val_marker,
su2double  val_origin 
)
inline

Set reference origin x-coordinate for moment computation.

Parameters
[in]val_marker- the marker we are monitoring.
[in]val_origin- New x-coordinate of the mesh motion origin.

Definition at line 597 of file config_structure.inl.

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◆ SetRefOriginMoment_Y()

void CConfig::SetRefOriginMoment_Y ( unsigned short  val_marker,
su2double  val_origin 
)
inline

Set reference origin y-coordinate for moment computation.

Parameters
[in]val_marker- the marker we are monitoring.
[in]val_origin- New y-coordinate of the mesh motion origin.

Definition at line 599 of file config_structure.inl.

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◆ SetRefOriginMoment_Z()

void CConfig::SetRefOriginMoment_Z ( unsigned short  val_marker,
su2double  val_origin 
)
inline

Set reference origin z-coordinate for moment computation.

Parameters
[in]val_marker- the marker we are monitoring.
[in]val_origin- New z-coordinate of the mesh motion origin.

Definition at line 601 of file config_structure.inl.

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◆ SetRestart_Bandwidth_Agg()

void CConfig::SetRestart_Bandwidth_Agg ( su2double  val_restart_bandwidth_sum)
inline

Set the sum of the bandwidth for writing binary restarts (to be averaged later).

Parameters
[in]Sumof the bandwidth for writing binary restarts.

Definition at line 1947 of file config_structure.inl.

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◆ SetReynolds()

void CConfig::SetReynolds ( su2double  val_reynolds)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 667 of file config_structure.inl.

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◆ SetRotation_Rate_Z()

void CConfig::SetRotation_Rate_Z ( su2double  newRotation_Rate_Z,
unsigned short  val_iZone 
)
inline

Set the angular velocity of the mesh about the z-axis.

Parameters
[in]val_iZone- Number for the current zone in the mesh (each zone has independent motion).
[in]newRotation_Rate_Z- new rotation rate after computing the ramp value.

Definition at line 938 of file config_structure.inl.

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◆ SetRunTime_Options()

void CConfig::SetRunTime_Options ( void  )

Set the config options.

Definition at line 635 of file config_structure.cpp.

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◆ SetRunTime_Parsing()

bool CConfig::SetRunTime_Parsing ( char  case_filename[MAX_STRING_SIZE])

Set the config file parsing.

Definition at line 2382 of file config_structure.cpp.

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◆ SetSemiSpan()

void CConfig::SetSemiSpan ( su2double  val_semispan)
inline

In case the SemiSpan is equal to 0 then, it is necessary to compute the max y distance, with this function we set the value of the semi span.

Parameters
[in]val_semispan- Value of the semispan.

Definition at line 428 of file config_structure.inl.

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◆ SetSmoothNumGrid()

void CConfig::SetSmoothNumGrid ( bool  val_smoothnumgrid)
inline

Set information about there is a smoothing of the grid coordinates.

Parameters
[in]val_smoothnumgrid- TRUE if there is smoothing of the grid coordinates; otherwise FALSE.

Definition at line 1599 of file config_structure.inl.

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◆ SetSpecific_Heat_Cp()

void CConfig::SetSpecific_Heat_Cp ( su2double  val_specific_heat_cp)
inline

Set the value of the specific heat at constant pressure (incompressible fluids with energy equation).

Parameters
[in]val_specific_heat_cp- specific heat at constant pressure.

Definition at line 691 of file config_structure.inl.

◆ SetSpecific_Heat_CpND()

void CConfig::SetSpecific_Heat_CpND ( su2double  val_specific_heat_cpnd)
inline

Set the non-dimensional value of the specific heat at constant pressure (incompressible fluids with energy equation).

Parameters
[in]val_specific_heat_cpnd- non-dim. specific heat at constant pressure.

Definition at line 639 of file config_structure.inl.

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◆ SetSpecific_Heat_Cv()

void CConfig::SetSpecific_Heat_Cv ( su2double  val_specific_heat_cv)
inline

Set the value of the specific heat at constant volume (incompressible fluids with energy equation).

Parameters
[in]val_specific_heat_cv- specific heat at constant volume.

Definition at line 693 of file config_structure.inl.

◆ SetSpecific_Heat_CvND()

void CConfig::SetSpecific_Heat_CvND ( su2double  val_specific_heat_cvnd)
inline

Set the non-dimensional value of the specific heat at constant volume (incompressible fluids with energy equation).

Parameters
[in]val_specific_heat_cvnd- non-dim. specific heat at constant pressure.

Definition at line 641 of file config_structure.inl.

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◆ SetSpline()

void CConfig::SetSpline ( vector< su2double > &  x,
vector< su2double > &  y,
unsigned long  n,
su2double  yp1,
su2double  ypn,
vector< su2double > &  y2 
)

Given arrays x[1..n] and y[1..n] containing a tabulated function, i.e., yi = f(xi), with x1 < x2 < . . . < xN , and given values yp1 and ypn for the first derivative of the interpolating function at points 1 and n, respectively, this routine returns an array y2[1..n] that contains the second derivatives of the interpolating function at the tabulated points xi. If yp1 and/or ypn are equal to 1 × 1030 or larger, the routine is signaled to set the corresponding boundary condition for a natural spline, with zero second derivative on that boundary. Numerical Recipes: The Art of Scientific Computing, Third Edition in C++.

Definition at line 8422 of file config_structure.cpp.

◆ SetSurface_DC60()

void CConfig::SetSurface_DC60 ( unsigned short  val_imarker,
su2double  val_surface_distortion 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 108 of file config_structure.inl.

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◆ SetSurface_Density()

void CConfig::SetSurface_Density ( unsigned short  val_imarker,
su2double  val_surface_density 
)
inline

Set the density at the surface.

Parameters
[in]val_imarker- Index corresponding to the outlet boundary.
[in]val_surface_density- Value of the density.

Definition at line 118 of file config_structure.inl.

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◆ SetSurface_Enthalpy()

void CConfig::SetSurface_Enthalpy ( unsigned short  val_imarker,
su2double  val_surface_enthalpy 
)
inline

Set the enthalpy at the surface.

Parameters
[in]val_imarker- Index corresponding to the outlet boundary.
[in]val_surface_density- Value of the density.

Definition at line 120 of file config_structure.inl.

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◆ SetSurface_IDC()

void CConfig::SetSurface_IDC ( unsigned short  val_imarker,
su2double  val_surface_distortion 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 138 of file config_structure.inl.

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◆ SetSurface_IDC_Mach()

void CConfig::SetSurface_IDC_Mach ( unsigned short  val_imarker,
su2double  val_surface_distortion 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 140 of file config_structure.inl.

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◆ SetSurface_IDR()

void CConfig::SetSurface_IDR ( unsigned short  val_imarker,
su2double  val_surface_distortion 
)
inline

Get the back pressure (static) at an outlet boundary.

Parameters
[in]val_index- Index corresponding to the outlet boundary.
Returns
The outlet pressure.

Definition at line 142 of file config_structure.inl.

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◆ SetSurface_Mach()

void CConfig::SetSurface_Mach ( unsigned short  val_imarker,
su2double  val_surface_mach 
)
inline

Set the mach number at the surface.

Parameters
[in]val_imarker- Index corresponding to the outlet boundary.
[in]val_surface_massflow- Value of the mach number.

Definition at line 112 of file config_structure.inl.

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◆ SetSurface_MassFlow()

void CConfig::SetSurface_MassFlow ( unsigned short  val_imarker,
su2double  val_surface_massflow 
)
inline

Set the massflow at the surface.

Parameters
[in]val_imarker- Index corresponding to the outlet boundary.
[in]val_surface_massflow- Value of the mass flow.

Definition at line 110 of file config_structure.inl.

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◆ SetSurface_MomentumDistortion()

void CConfig::SetSurface_MomentumDistortion ( unsigned short  val_imarker,
su2double  val_surface_momentumdistortion 
)
inline

Set the momentum distortion at the surface.

Parameters
[in]val_imarker- Index corresponding to the outlet boundary.
[in]val_surface_momentumdistortion- Value of the momentum distortion.

Definition at line 130 of file config_structure.inl.

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◆ SetSurface_NormalVelocity()

void CConfig::SetSurface_NormalVelocity ( unsigned short  val_imarker,
su2double  val_surface_normalvelocity 
)
inline

Set the normal velocity at the surface.

Parameters
[in]val_imarker- Index corresponding to the outlet boundary.
[in]val_surface_normalvelocity- Value of the normal velocity.

Definition at line 122 of file config_structure.inl.

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◆ SetSurface_Pressure()

void CConfig::SetSurface_Pressure ( unsigned short  val_imarker,
su2double  val_surface_pressure 
)
inline

Set the pressure at the surface.

Parameters
[in]val_imarker- Index corresponding to the outlet boundary.
[in]val_surface_massflow- Value of the pressure.

Definition at line 116 of file config_structure.inl.

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◆ SetSurface_PressureDrop()

void CConfig::SetSurface_PressureDrop ( unsigned short  val_imarker,
su2double  val_surface_pressuredrop 
)
inline

Set the pressure drop between two surfaces.

Parameters
[in]val_imarker- Index corresponding to the outlet boundary.
[in]val_surface_pressuredrop- Value of the pressure drop.

Definition at line 136 of file config_structure.inl.

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◆ SetSurface_SecondaryStrength()

void CConfig::SetSurface_SecondaryStrength ( unsigned short  val_imarker,
su2double  val_surface_secondarystrength 
)
inline

Set the secondary flow strength at the surface.

Parameters
[in]val_imarker- Index corresponding to the outlet boundary.
[in]val_surface_secondarystrength- Value of the secondary flow strength.

Definition at line 126 of file config_structure.inl.

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◆ SetSurface_SecondOverUniform()

void CConfig::SetSurface_SecondOverUniform ( unsigned short  val_imarker,
su2double  val_surface_secondaryoverstream 
)
inline

Set the relative secondary flow strength at the surface.

Parameters
[in]val_imarker- Index corresponding to the outlet boundary.
[in]val_surface_secondaryoverstream- Value of the relative seondary flow strength.

Definition at line 128 of file config_structure.inl.

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◆ SetSurface_Temperature()

void CConfig::SetSurface_Temperature ( unsigned short  val_imarker,
su2double  val_surface_temperature 
)
inline

Set the temperature at the surface.

Parameters
[in]val_imarker- Index corresponding to the outlet boundary.
[in]val_surface_massflow- Value of the temperature.

Definition at line 114 of file config_structure.inl.

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◆ SetSurface_TotalPressure()

void CConfig::SetSurface_TotalPressure ( unsigned short  val_imarker,
su2double  val_surface_totalpressure 
)
inline

Set the total pressure at the surface.

Parameters
[in]val_imarker- Index corresponding to the outlet boundary.
[in]val_surface_totalpressure- Value of the total pressure.

Definition at line 134 of file config_structure.inl.

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◆ SetSurface_TotalTemperature()

void CConfig::SetSurface_TotalTemperature ( unsigned short  val_imarker,
su2double  val_surface_totaltemperature 
)
inline

Set the total temperature at the surface.

Parameters
[in]val_imarker- Index corresponding to the outlet boundary.
[in]val_surface_totaltemperature- Value of the total temperature.

Definition at line 132 of file config_structure.inl.

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◆ SetSurface_Uniformity()

void CConfig::SetSurface_Uniformity ( unsigned short  val_imarker,
su2double  val_surface_streamwiseuniformity 
)
inline

Set the streamwise flow uniformity at the surface.

Parameters
[in]val_imarker- Index corresponding to the outlet boundary.
[in]val_surface_streamwiseuniformity- Value of the streamwise flow uniformity.

Definition at line 124 of file config_structure.inl.

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◆ SetTemperature_FreeStream()

void CConfig::SetTemperature_FreeStream ( su2double  val_temperature_freestream)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 633 of file config_structure.inl.

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◆ SetTemperature_FreeStreamND()

void CConfig::SetTemperature_FreeStreamND ( su2double  val_temperature_freestreamnd)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 635 of file config_structure.inl.

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◆ SetTemperature_Ref()

void CConfig::SetTemperature_Ref ( su2double  val_temperature_ref)
inline

Set the reference temperature.

Returns
Value of the Froude number.

Definition at line 679 of file config_structure.inl.

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◆ SetThermal_Expansion_Coeff()

void CConfig::SetThermal_Expansion_Coeff ( su2double  val_thermal_expansion)
inline

Set the thermal expansion coefficient.

Parameters
[in]val_thermal_expansion- thermal expansion coefficient

Definition at line 695 of file config_structure.inl.

◆ SetThermal_Expansion_CoeffND()

void CConfig::SetThermal_Expansion_CoeffND ( su2double  val_thermal_expansionnd)
inline

Set the non-dim. thermal expansion coefficient.

Parameters
[in]val_thermal_expansion- non-dim. thermal expansion coefficient

Definition at line 643 of file config_structure.inl.

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◆ SetThermalDiffusivity_Solid()

void CConfig::SetThermalDiffusivity_Solid ( su2double  val_thermal_diffusivity)
inline

Set the thermal diffusivity for solids.

Returns
Value of the Froude number.

Definition at line 705 of file config_structure.inl.

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◆ SetTime_Ref()

void CConfig::SetTime_Ref ( su2double  val_time_ref)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 681 of file config_structure.inl.

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◆ SetTke_FreeStream()

void CConfig::SetTke_FreeStream ( su2double  val_tke_freestream)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 655 of file config_structure.inl.

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◆ SetTke_FreeStreamND()

void CConfig::SetTke_FreeStreamND ( su2double  val_tke_freestreamnd)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 651 of file config_structure.inl.

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◆ SetTotal_UnstTimeND()

void CConfig::SetTotal_UnstTimeND ( su2double  val_total_unsttimend)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 663 of file config_structure.inl.

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◆ SetTotalTemperatureIn_BC()

void CConfig::SetTotalTemperatureIn_BC ( su2double  val_temp)

Set the inlet total temperature imposed as BC for internal flow.

Parameters
[in]val_temp- New value of the total temperature.

Definition at line 7854 of file config_structure.cpp.

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◆ SetTranspirationParams_DV()

void CConfig::SetTranspirationParams_DV ( )

Set the transpiration params using DV values.

Parameters
[in]val_index- Index corresponding to the transpiration boundary.

Definition at line 8019 of file config_structure.cpp.

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◆ SetUpdate_AoA()

void CConfig::SetUpdate_AoA ( bool  val_update)
inline

Set the value of the boolean for updating AoA in fixed lift mode.

Parameters
[in]val_update- the bool for whether to update the AoA.

Definition at line 1775 of file config_structure.inl.

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◆ SetUpdate_BCThrust_Bool()

void CConfig::SetUpdate_BCThrust_Bool ( bool  val_update)
inline

Set the value of the boolean for updating AoA in fixed lift mode.

Parameters
[in]val_update- the bool for whether to update the AoA.

Definition at line 1779 of file config_structure.inl.

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◆ SetVelocity_FreeStream()

void CConfig::SetVelocity_FreeStream ( su2double  val_velocity_freestream,
unsigned short  val_dim 
)
inline

Set the free-stream velocity.

Parameters
[in]val_velocity_freestream- Value of the free-stream velocity component.
[in]val_dim- Value of the current dimension.

Definition at line 645 of file config_structure.inl.

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◆ SetVelocity_FreeStreamND()

void CConfig::SetVelocity_FreeStreamND ( su2double  val_velocity_freestreamnd,
unsigned short  val_dim 
)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 647 of file config_structure.inl.

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◆ SetVelocity_Ref()

void CConfig::SetVelocity_Ref ( su2double  val_velocity_ref)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 673 of file config_structure.inl.

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◆ SetViscosity_FreeStream()

void CConfig::SetViscosity_FreeStream ( su2double  val_viscosity_freestream)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 627 of file config_structure.inl.

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◆ SetViscosity_FreeStreamND()

void CConfig::SetViscosity_FreeStreamND ( su2double  val_viscosity_freestreamnd)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 649 of file config_structure.inl.

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◆ SetViscosity_Ref()

void CConfig::SetViscosity_Ref ( su2double  val_viscosity_ref)
inline

Set the Froude number for free surface problems.

Returns
Value of the Froude number.

Definition at line 699 of file config_structure.inl.

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◆ SetWeight_ObjFunc()

void CConfig::SetWeight_ObjFunc ( unsigned short  val_obj,
su2double  val 
)
inline

Set the weight of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc.

Author
H. Kline
Note
The objective function will determine the boundary condition of the adjoint problem.
Returns
Weight of objective function.

Definition at line 1278 of file config_structure.inl.

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◆ SetWrt_Con_Freq()

void CConfig::SetWrt_Con_Freq ( unsigned long  val_freq)
inline

Set the frequency for writing the convergence file.

Returns
It writes the convergence file with this frequency.

Definition at line 840 of file config_structure.inl.

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◆ SetWrt_InletFile()

void CConfig::SetWrt_InletFile ( bool  val_wrt_inletfile)
inline

Set information about writing a template inlet profile file.

Parameters
[in]val_wrt_inletfile- flag for whether to write a template inlet profile file.

Definition at line 1673 of file config_structure.inl.

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◆ SubtractFinestMesh()

void CConfig::SubtractFinestMesh ( void  )
inline

Subtract one to the index of the finest grid (full multigrid strategy).

Returns
Change the index of the finest grid.

Definition at line 735 of file config_structure.inl.

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◆ Tick()

void CConfig::Tick ( double *  val_start_time)

Start the timer for profiling subroutines.

Parameters
[in]val_start_time- the value of the start time.

Definition at line 8477 of file config_structure.cpp.

◆ Tock()

void CConfig::Tock ( double  val_start_time,
string  val_function_name,
int  val_group_id 
)

Stop the timer for profiling subroutines and store results.

Parameters
[in]val_start_time- the value of the start time.
[in]val_function_name- string for the name of the profiled subroutine.
[in]val_group_id- string for the name of the profiled subroutine.

Definition at line 8490 of file config_structure.cpp.

◆ TokenizeString()

bool CConfig::TokenizeString ( string &  str,
string &  option_name,
vector< string > &  option_value 
)

breaks an input line from the config file into a set of tokens

Parameters
[in]str- the input line string
[out]option_name- the name of the option found at the beginning of the line
[out]option_value- the tokens found after the "=" sign on the line
Returns
false if the line is empty or a commment, true otherwise

Definition at line 6307 of file config_structure.cpp.

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Member Data Documentation

◆ fields

vector<string> CConfig::fields

Tags for the different fields in a restart file.

Definition at line 1369 of file config_structure.hpp.


The documentation for this class was generated from the following files: